1. Hartman, Edwin P.: Adventures in Research: A History of Ames Research Center, 1940-1965. NASA SP-4302, 1970.
2. Rodert, Lewis A.; McAvoy, William H.; and Clousing, Lawrence A.: Preliminary Report on Flight Tests of an Airplane Having Exhaust Heated Wings. NACA Wartime Report A-53, 1941.
3. Look, Bonne C.: Flight Tests of the Thermal Ice-Protection Equipment on the B-17F Airplane. NACA Wartime Report A-23, 1944.
4. Selna, James; Neel, Carr B., Jr.; and Zeiller, E. Lewis: An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane. IV. Results of Flight Tests in Dry-Air and Natural-Icing Conditions. NACA Wartime Report A-22, 1945.
5. Neel, Carr B., Jr.; and Bright, Loren G.: The Effect of Ice Formations on Propeller Performance. NACA TN-2212, 1950.
6. Jones, Alun R.: An Investigation of a Thermal Ice-Prevention System for a Twin-Engine Transport Airplane. NACA Report 862, 1946.
7. Rathert, George A., Jr.; Hanson, Carl M.; and Rolls, L. Stewart: Investigation of a Thin Straight Wing of Aspect Ratio 4 by the NACA Wing-Flow Method: Lift and Pitching Moment Characteristics of the Wing Alone. NACA RM-A8L20, 1949.
8. Rathert, George A., Jr.; and Cooper, George E.: Wing-Flow Tests of a Triangular Wing of Aspect Ratio Two. I. Effectiveness of Several Types of Trailing-Edge Flaps on Flat-Plate Models. NACA RM-A7G18, 1947.
9. Nissen, James M.; Gadeberg, Burnett L.; and Hamilton, William T.: Correlation of the Drag Characteristics of a Typical Pursuit Airplane Obtained from High-Speed Wind Tunnel and Flight Tests. NACA Report 916, 1948.
10. Clousing, Lawrence A.; and Turner, William N.: Flight Measurements of Horizontal Tail Loads on a Typical Propeller-Driven Pursuit Airplane during Stalled Pull-Outs at High Speed. NACA Wartime Report A-81, 1944.
11. Clousing, Lawrence A.; Turner, William N.; and Rolls, L. Stewart: Measurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit-Type Airplane at Several Values of Mach Number. NACA TR-859, 1946.
12. Sadoff, Melvin; Turner, William N.; and Clousing, Lawrence A.: Measurements of the Pressure Distribution on the Horizontal-Tail Surface of a Typical Propeller Driven Pursuit Airplane in Flight: Effects of Compressibility in Steady Straight and Accelerated Flight. NACA TN-1144, 1947.
13. Turner, William N.; Steffen, Paul J.; and Clousing, Lawrence A.: Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-Type Airplane As Measured in Flight. NACA Report 854, 1946.
14. White, Maurice D.; Lomax, Harvard; and Turner, Howard L.: Sideslip Angles and Vertical-Tail Loads in Rolling Pull-Out Maneuvers. NACA TN-1122, 1947.
15. Gasich, Welko E.; and Clousing, Lawrence A.: Flight Investigation of the Variation of Drag Coefficient with Mach Number for the Bell P-39N-1 Airplane. NACA Wartime Report A-61, 1945.
16. Cooper, George E.; and Rathert, George A., Jr.: Visual Observation of the Shock Wave in Flight. NACA RM-A8C25, 1948.
17. Cooper, George E.; and Bray, Richard S.: Schlieren Investigation of the Wing Shock-Wave Boundary-Layer Interaction in Flight. NACA RM-A51G09, 1951.
18. White, Maurice D.; Sadoff, Melvin; Clousing, Lawrence A.; and Cooper, George E.: Preliminary Results of a Flight Investigation to Determine the Effect of Negative Flap Deflection on High-Speed Longitudinal Control Characteristics. NACA RM-A7I26, 1947.
19. Gasich, Welko E.: Experimental Verification of Two Methods for Computing the Takeoff Ground Run of Propeller-Driven Aircraft. NACA TN 1258, 1947.
20. Clousing, Lawrence A.; Brown, Harvey H.; and Rathert, George A.: Flight-Test Measurements of Aileron Control Surface Behaviour at Supercritical Mach Numbers. NACA RM-A7A15, 1947.
21. Brown, Harvey H.; and Clousing, Lawrence A.: Wing Pressure-Distribution Measurements Up to 0.866 Mach Number in Flight on a Jet-Propelled Airplane. NACA TN-1181, 1947.
22. Spreiter, John R.; Galster, George M.; and Cooper, George E.: Flight Observations of Aileron Flutter at High Mach Number As Affected by Several Modifications. NACA RM-A7B03, 1947.
23. Clousing, Lawrence A.: Precautions for Flight Testing Near the Speed of Sound. NACA RM-A7G25, 1947.
24. Spreiter, John R.; and Steffan, Paul J.: Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient. NACA TN-1044, 1946.
25. Anderson, Seth B.; and Bray, Richard S.: A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-Up of a Swept-Wing Airplane in Maneuvering Flight at Transonic Speeds. NACA-TR-1237, 1955.
26. McFadden, Norman M.; and Heinle, Donovan R.: Flight Investigation of the Effects of Horizontal-Tail Height, Moment of Inertia, and Control Effectiveness on the Pitch-Up Characteristics of a 35 deg Swept-Wing Fighter Airplane at High Subsonic Speeds. NACA RM-A54F21, 1955.
27. Anderson, Seth B.; Matteson, Frederick H.; and Van Dyke, Rudolph D., Jr.: A Flight Investigation of the Effect of Leading-Edge Camber on the Aerodynamic Characteristics of a Swept-Wing Airplane. NACA RM-A52L16a, 1953.
28. Matteson, Frederick H.; and Van Dyke, Rudolph D., Jr.: Flight Investigation of the Effects of a Partial-Span Leading-Edge Chord Extension on the Aerodynamic Characteristics of a 35 deg Swept-Wing Fighter Airplane. NACA RM-A54B26, 1954.
29. Sadoff, Melvin; Stewart, John D.; and Cooper, George E.: Analytical Study of Comparative Pitch-Up Behavior of Several Airplanes and Correlation with Pilot Opinion. NACA RM-A57D04, 1957.
30. Rathert, George A., Jr.; Winograd, Lee; Cooper, George E.; and Rolls, L. Stewart: Preliminary Flight Investigation of the Wing-Dropping Tendency and Lateral Control Characteristics of a 35 deg Swept-Wing Airplane at Transonic Mach Numbers. NACA RM-A50H03, 1950.
31. McFadden, Norman M.; Rathert, George A., Jr.; and Bray, Richard S.: The Effectiveness of Wing Vortex Generators in Improving the Maneuvering Characteristics of a Swept-Wing Airplane at Transonic Speeds. NACA TN-3523, 1955.
32. Bray, Richard S.: The Effects of Fences on the High-Speed Longitudinal Stability of a Swept-Wing Airplane. NACA RM-A53F23, 1953.
33. Rolls, L. Stewart: A Flight Comparison of a Submerged Inlet and a Scoop Inlet at Transonic Speeds. NACA RM-A53A06, 1953.
34. Rolls, L. Stewart; Havill, C. Dewey; and Holden, George R.: Techniques for Determining Thrust In-Flight for Airplanes Equipped with Afterburners. NACA RM-A52K12, 1953.
35. Rolls, L. Stewart; and Wingrove, Rodney C.: An Investigation of the Drag Characteristics of a Tailless Delta-Wing Airplane in Flight, Including Comparison with Wind-Tunnel Data. NACA Memo 10-8-58A, Nov. 1958.
36. Rolls, L. Stewart; Koenig, David G.; and Drinkwater, Fred J., III: Flight Investigation of the Aerodynamic Properties of an Ogee Wing. NASA TN D-3071, 1965.
37. Jacobsen, Robert A.; and Short, Barbara J.: A Flight Investigation of the Wake Turbulence Alleviation Resulting from a Flap Configuration Change on a B-747 Aircraft. NASA TM-73,263, 1977.
38. Tinling, Bruce E.: Estimation of Vortex-Induced Roll Excursions Based on Flight and Simulation Results. In: FAA-RD-77-68 Proceedings of the Aircraft Wake Vortices Conference, Mar. 1977, pp. 11-22.
39. Short, Barbara J.; and Jacobsen, Robert A.: Evaluation of a Wake Vortex Upset Model Based on Simultaneous Measurements of Wake Velocities and Probe-Aircraft Accelerations. NASA TM-78561, 1979.
40. Turner, Howard L.; and Cooper, George E.: Partial Measurements in Flight of the Flying Qualities of a Grumman XF7F-1 Airplane with a Modified Vertical Tail. NACA RM-A7D15, 1947.
41. Spahr, J. Richard; and Christopherson, Don R.: Measurements in Flight of the Stability, Lateral Control, and Stalling Characteristics of an Airplane Equipped with Full Span Flaps and Spoiler-Type Ailerons. NACA Wartime Report A-28, Dec. 1943.
42. Hanson, Carl M.; and Anderson, Seth B.: Flight Tests of a Double-Hinged Horizontal Tail Surface with Reference to Longitudinal-Stability and -Control Characteristics. NACA TN-1224, 1947.
43. Cole, Henry A., Jr.; and Holleman, Euclid C.: Measured and Predicted Dynamic Response Characteristics of a Flexible Airplane to Elevator Control over a Frequency Range Including Three Structural Modes. NACA TN-4147, 1958.
44. Cole, Henry A., Jr.; Brown, Stuart C.; and Holleman, Euclid C.: Experimental and Predicted Longitudinal and Lateral-Directional Response Characteristics of a Large Flexible 358 Swept-Wing Airplane at an Altitude of 35,000 Feet. NACA Report 1330, 1957.
45. Goett, Harry J.; Jackson, Roy P.; and Belsley, Steven E.: Wind-Tunnel Procedure for Determination of Critical Stability and Control Characteristics of Airplanes. NACA Report 781, 1944.
46. Delany, Noel K.; and Kauffman, William M.: Correlation of Wind-Tunnel Predictions with Flight Tests of a Twin-Engine Patrol Airplane. I. Longitudinal- Stability and -Control Characteristics. NACA Wartime Report A-86, 1945.
47. Delany, Noel K.; and Kauffman, William M.: Correlation of Wind-Tunnel Predictions with Flight Tests of a Twin-Engine Patrol Airplane. II. Lateral- and Directional-Stability and -Control Characteristics. NACA Wartime Report A-71, 1945.
48. Anderson, Seth B.; Christofferson, Frank E.; and Clousing, Lawrence A.: Flight Measurement of the Flying Qualities of a Lockheed P-80A Airplane: Longitudinal Stability and Control Characteristics. NACA RM-A7G01, 1947.
49. Anderson, Seth B.; and Cooper, George E.: Flight Measurements of the Flying Qualities of a Lockheed P-80A Airplane: Lateral- and Directional-Stability and -Control Characteristics. NACA RM-A7J24, 1947.
50. Heinle, Donovan R.; and McNeill, Walter E.: Correlation of Predicted and Experimental Lateral Oscillation Characteristics for Several Airplanes. NACA RM-A52J06, 1952.
51. Anderson, Seth B.: Correlation of Flight and Wind-Tunnel Measurements of Roll-Off in Low-Speed Stalls on a 35 deg Swept-Wing Aircraft. NACA RM-A53G22, 1953.
52. Sadoff, Melvin; Matteson, Frederick H.; and Van Dyke, Rudolph D., Jr.: The Effect of Blunt-Trailing-Edge Modifications on the High-Speed Stability and Control Characteristics of a Swept-Wing Fighter Airplane. NACA RM-A54C31, 1954.
53. McNeill, Walter E.; and Cooper, George E.: A Comparison of the Measured and Predicted Lateral Oscillatory Characteristics of a 35 deg Swept-Wing Fighter Airplane. NACA TN-3521, 1955.
54. Anderson, Seth B.; and Bray, Richard S.: A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-Up of a Swept-Wing Airplane in Maneuvering Flight at Transonic Speeds. NACA Report 1237, 1955.
55. Sadoff, Melvin: The Effects of Longitudinal Control-System Dynamics on Pilot Opinion and Response Characteristics as Determined from Flight Tests and from Ground Simulator Studies. NASA Memo 10-1-58A, 1958.
56. White, Maurice D.; and Innis, Robert C.: A Flight Investigation of Low Speed Handling Qualities of a Tailless Delta-Wing Fighter Airplane. NASA Memo 4-15-59A, May 1959.
57. McNeill, Walter E.; and Innis, Robert C.: A Simulator and Flight Study of Yaw Coupling in Turning Maneuvers of Large Transport Aircraft. NASA TN D-3910, 1967.
58. White, Maurice D.; Schlaff, Bernard A.; and Drinkwater, Fred J., III: A Comparison of Flight-Measured Carrier-Approach Speeds with Values Predicted by Several Different Criteria for 41 Fighter-Type Airplane Configurations. NACA RM-A57L11, 1958.
59. Drinkwater, Fred J., III; and Cooper, George E.: A Flight Evaluation of the Factors Which Influence the Selection of Landing Approach Speeds. NASA Memo 10-6-58A, Dec. 1958.
60. Innis, Robert C.: Factors Limiting the Landing Approach Speed of Airplanes from the Viewpoint of a Pilot. AGARD Report 358, 1961.
61. Creer, Brent Y.; Stewart, John D.; Merrick, Robert B.; and Drinkwater, Fred J., III: Pilot Opinion Study of Lateral Control Requirements for Fighter-Type Aircraft. NASA Memo 1-29-59A, Mar. 1959.
62. Cooper, George E.: Understanding and Interpreting Pilot Opinion. Aeronautical Engineering Review, vol. 16, no. 3, Mar. 1957, pp. 47-51.
63. Cooper, George E.; and Harper, Robert P., Jr.: The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities. NASA TN D-5153, 1969.
64. Kauffman, William M.; Liddell, Charles J., Jr.; Smith, G. Allan; and Van Dyke, Rudolph D., Jr.: An Apparatus for Varying Effective Dihedral in Flight with Application to a Study of Tolerable Dihedral on a Conventional Fighter Airplane. NACA Report 948, 1949.
65. McNeill, Walter E.; and Creer, Brent Y.: A Summary of Results Obtained during Flight Simulation of Several Aircraft Prototypes with Variable Stability Airplanes. NACA RM-A56C08, 1956.
66. Liddell, Charles J., Jr.; Van Dyke, Rudolph D., Jr.; and Heinle, Donovan R.: A Flight Determination of the Tolerable Range of Effective Dihedral on a Conventional Fighter Airplane. NASA TN-1936, 1949.
67. Liddell, Charles J., Jr.; Creer, Brent Y.; and Van Dyke, Rudolph D., Jr.: A Flight Study of Requirements for Satisfactory Lateral Oscillatory Characteristics of Fighter Aircraft. NACA RM-A51E16, 1951.
68. McNeill, Walter E.; Drinkwater, Fred J., III; and Van Dyke, Rudolph D., Jr.: A Flight Study of the Effects on Tracking Performance of Changes in the Lateral-Oscillatory Characteristics of a Fighter Airplane. NACA RM-A53H10, 1953.
69. McNeill, Walter E.; and Vomaske, Richard F.: A Flight Investigation to Determine the Lateral Oscillatory Damping Acceptable for an Airplane in the Landing Approach. NASA Memo 12-10-58A, Feb. 1959.
70. Vomaske, Richard F.; Sadoff, Melvin; and Drinkwater, Fred J., III: The Effect of Lateral-Directional Control Coupling on Pilot Control of an Airplane as Determined in Flight and a Fixed-Base Flight Simulator. NASA TN D-1141, 1961.
71. McFadden, Norman M.; Pauli, Frank A.; and Heinle, Donovan R.: A Flight Study of Longitudinal Control-System Dynamic Characteristics by the Use of a Variable Control-System Airplane. NACA RM-A57L10, 1958.
72. McFadden, Norman M.; Vomaske, Richard F.; and Heinle, Donovan R.: Flight Investigation Using Variable Stability Airplanes of Minimum Stability Requirements for High-Speed, High-Altitude Vehicles. NASA TN D-779, 1961.
73. Kauffman, William M.; and Drinkwater, Fred J., III: Variable Stability Airplanes in Lateral Stability Research. Aeronautical Engineering Review, vol. 14, no. 8, Aug. 1955, pp. 29-35.
74. Foster, John V.: Servomechanisms as Used on Variable-Stability and Variable-Control-System Research Aircraft. Proceedings of the National Electronics Conference, Oct. 1957, pp. 167-177.
75. McNeill, Walter E.; Gerdes, Ronald M.; Innis, Robert C.; and Ratcliff, Jack D.: A Flight Study of the Use of Direct-Lift-Control Flaps to Improve Station Keeping during In-Flight Refueling. NASA TM X-2936, 1973.
76. Rathert, George A., Jr.; Gadeberg, Burnett L.; and Ziff, Howard L.: An Analysis of the Tracking Performances of Two Straight-Wing and Two Swept-Wing Fighter Aircraft with Fixed Sights in Standardized Test Maneuver. NACA RM-A53H12, 1953.
77. Gadeberg, Burnett L.; and Rathert, George A., Jr.: Tracking Performance of a Swept-Wing Fighter With a Disturbed Reticle Lead-Computing Sight. NACA RM-A54K16, 1959.
78. Rathert, George A., Jr.; Abramovitz, M.; and Gadeberg, B. L.: The Effects of Powered Controls and Fire Control Systems on Tracking Accuracy. NACA RM-A55D12a, 1955.
79. Doolin, Brian; Smith, G. Allan; and Drinkwater, Fred J., III: An Air-Borne Target Simulator for Use in Optical-Sight Tracking Studies. NACA RM-A55F20, 1955.
80. Douvillier, Joseph G., Jr.; Foster, John V.; and Drinkwater, Fred J., III: An Airborne Simulator Investigation of the Accuracy of an Optical Track Command Missile Guidance System. NACA RM-A56G24, 1956.
81. Foster, John V.; Fulcher, Elmer C.; and Heinle, Donovan R.: An Airborne Target Simulator for Use with Scope-Presentation Type Fire-Control Systems. NACA RM-A57C19, 1957.
82. Turner, Howard L.; White, John S.; and Van Dyke, Rudolph D., Jr.: Flight Testing by Radio Remote Control-Flight Evaluation of a Beep-Control System. NACA TN-3496, 1955.
83. Turner, Howard L.; Triplett, William C.; and White, John S.: A Flight and Analog Computer Study of Some Stabilization and Command Networks for an Automatically Controlled Interceptor during the Final Attack Phase. NACA RM-A54J14, 1955.
84. McNeill, Walter E.; McLean, John D.; Hegarty, Daniel M.; and Heinle, Donovan R.: Design and Flight Tests of an Adaptive Control System Employing Normal-Acceleration Command. NASA TN D-858, 1961.
85. Kibort, Bernard R.; and Drinkwater, Fred J., III: A Flight Study of Manual Blind Landing Performance Using Closed Circuit Television Displays. NASA TN D-2252, 1964.
86. Bray, Richard S.: A Head-Up Display Format for Application to Transport Aircraft Approach and Landing. NASA TM-81199, 1980.
87. McGee, Leonard A.; Smith, Gerald L.; Hegarty, Daniel M.; Carson, Thomas M.; Merrick, Robert B.; Schmidt, Stanley F.; and Conrad, Bjorn: Flight Results from a Study of Aided Inertial Navigation Applied to Landing Operations. NASA TN D-7302, 1973.
88. Lee, Homer Q.; Newman, Frank; and Hardy, Gordon H.: 4D Area Navigation System Description and Flight Test Results. NASA TN D-7874, 1975.
89. Erzberger, Heinz: Automation of On-Board Flightpath Management. NASA TM-84212, 1981.
90. Denery, Dallas G.; Callas, George P.; Hardy, Gordon H.; and Nedell, William: Design, Development and Flight Test of a Demonstration Advanced Avionics System. AGARD Conference Proceedings No. 34, 1983.
91. Paielli, Russell A.; Bach, Ralph E.; McNally, B. David; Simmons, Rickey C.; Warner, David N.; Forsyth, Theodore J.; Kanning, Gerd; Ahtye, C. T.; Kaufmann, D. N.; and Walton, J. C.: Carrier Phase Differential GPS Integrated with an Inertial Navigation System: Flight Test Evaluation with Auto-Coupled Precision Landing Guidance. Proceedings of The Institute of Navigation's 1995 National Technical Meeting, Jan. 1995, pp. 711-724.
92. Triplett, William C.; Brown, Stuart C.; and Smith, G. Allan: The Dynamic-Response Characteristics of a 35 deg Swept-Wing Airplane as Determined from Flight Measurements. NACA Report 1250, 1955.
93. Denery, Dallas G.: An Identification Algorithm That Is Insensitive to Initial Parameter Estimates. AIAA Journal, vol. 9, no. 3, Mar. 1971, pp. 371-377.
94. Bach, Ralph E., Jr.; and Wingrove, Rodney C.: Applications of State Estimation in Aircraft Flight Data Analysis. AIAA-83-2087, Aug. 1983.
95. Tischler, Mark B.: System Identification Methods for Aircraft Flight Control Development and Validation. NASA TM-110369, Oct. 1995.
96. Anderson, Seth B.; Cooper, George E.; and Faye, Alan, E., Jr.: Flight Measurements of the Effect of a Controllable Thrust Reverser on the Flight Characteristics of a Single-Engine Jet Airplane. NASA Memo 4-26-59A, 1959.
97. Bray, Richard S.; Snyder, C. Thomas; and Drinkwater, Fred J., III: A Preliminary Flight and Simulator Study of the Use of Wing Spoilers for Direct Lift Control in the Approach and Landing of a Jet Transport Airplane. Ames Research Center Working Paper 224.
98. Bray, Richard S.; Drinkwater, Fred J., III; and White, Maurice D.: A Flight Study of a Power-Off Landing Technique Applicable to Re-Entry Vehicles. NASA TN D-323, July 1960.
99. Edwards, Fred G.; Foster, John D.; Hegarty, Daniel M.; Smith, Donald W.; Drinkwater III, Fred J.; and Wingrove, Rodney C.: Flight Performance of a Navigation, Guidance and Control System Concept for Automatic Approach and Landing of the Space Shuttle Orbiter. NASA TN D-7899, 1975.
100. Edwards, Fred G.; Foster, John D.; Hegarty, Daniel M.; and Drinkwater III, Fred J.: Delayed Flap Approach Procedures for Noise Abatement and Fuel Conservation. Proceedings of the NASA Aircraft Safety and Operating Problems Conference, Oct. 1976, pp. 77-90.
101. Denery, Dallas G.; Bourquin, Kent R.; White, Kenneth C.; and Drinkwater, Fred J. III: Flight Evaluation of Three-Dimensional Area Navigation for Jet Transport Noise Abatement. Journal of Aircraft, vol. 10, no. 4, Apr. 1973, pp. 226-231.
102. Holzhauser, Curt A.; and Bray, Richard S.: Wind Tunnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 deg Swept-Wing Airplane. NACA Report 1276, 1956.
103. Cook, Woodrow; Anderson, Seth B.; and Cooper, George E.: Area-Suction Boundary-Layer Control as Applied to the Trailing-Edge Flaps of a 35 deg Swept-Wing Airplane. NACA Report 1370, 1958.
104. Kelly, Mark W.; Anderson, Seth B.; and Innis, Robert C.: Blowing-Type Boundary-Layer Control as Applied to the Trailing-Edge Flaps of a 35 deg Swept-Wing Airplane. NACA Report 1369, 1958.
105. Quigley, Hervey C.; Anderson, Seth B.; and Innis, Robert C.: Flight Investigation of the Low-Speed Characteristics of a 45 deg Swept-Wing Fighter-Type Airplane with Blowing Boundary-Layer Control Applied to the Leading- and Trailing-Edge Flaps. NASA TN D-321, 1960.
106. Rolls, L. Stewart; Cook, Anthony M.; and Innis, Robert C.: Flight-Determined Aerodynamic Properties of a Jet-Augmented, Auxiliary-Flap, Direct Lift-Control System Including Correlation with Wind-Tunnel Results. NASA TN D-5128, 1969.
107. Quigley, Hervey C.; and Innis, Robert C.: Handling Qualities and Operational Problems of a Large Four-Propeller STOL Transport Airplane. NASA TN D-1647, 1963.
108. Quigley, Hervey C.; Innis, Robert C.; Vomaske, Richard F.; and Ratcliff, Jack W.: A Flight and Simulator Study of Directional Augmentation Criteria for a Four-Propellered STOL Airplane. NASA TN D-3909, 1967.
109. Quigley, Hervey C.; Innis, Robert C.; and Holzhauser, Curt A.: A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers. NASA TN D-2231, 1964.
110. Innis, Robert C.; Holzhauser, Curt A.; and Gallant, Richard P.: Flight Tests under IFR with a STOL Transport Aircraft. NASA TN D-4939, 1968.
111. Holzhauser, Curt A.; Innis, Robert C.; and Vomaske, Richard F.: A Flight and Simulator Study of the Handling Qualities of a Deflected Slipstream STOL Seaplane Having Four Propellers and Boundary-Layer Control. NASA TN D-2966, 1965.
112. Innis, Robert C.; Holzhauser, Curt A.; and Quigley, Hervey C.: Airworthiness Considerations for STOL Aircraft. NASA TN D-5594, 1970.
113. Few, David D.: A Perspective on 15 Years of Proof of Concept Aircraft Development and Flight Research at Ames-Moffett by the Rotorcraft and Powered-Lift Flight Projects Division, 1970-1985. NASA Reference Publication 1187, 1987.
114. Weiberg, James A.; Giulianetti, Demo; Gambucci, Bruno; and Innis, Robert C.: Takeoff and Landing Performance and Noise Characteristics of a Deflected Slipstream STOL Airplane with Interconnected Propellers and Rotating Cylinder Flaps. NASA TM X-62,320, 1973.
115. Quigley, Hervey C.; Innis, Robert C.; and Grossmith, S.: A Flight Investigation of the STOL Characteristics of an Augmented Jet Flap STOL Research Aircraft. NASA TM X-62,334, 1974.
116. Vomaske, Richard F.; Innis, Robert C.; Swan, Brian E.; and Grossmith, Seth W.: A Flight Investigation of the Stability, Control, and Handling Qualities of an Augmented Jet Flap STOL Airplane. NASA TP-1254, 1978.
117. Stephenson, Jack D.: The Application of Parameter Estimation to Flight Measurements to Obtain Lateral-Directional Stability Derivatives of an Augmented Jet-Flap STOL Airplane. NASA TP-2033, 1983.
118. Franklin, James A.; Innis, Robert C.; Hardy, Gordon H.; and Stephenson, Jack D.: Design Criteria for Flightpath and Airspeed Control for the Approach and Landing of STOL Aircraft. NASA TP-1911, 1982.
119. Hindson, William S.; Hardy, Gordon H.; and Innis, Robert C.: Flight-Test Evaluation of STOL Control and Flight Director Concepts in a Powered-Lift Aircraft Flying Curved Decelerating Approaches. NASA TP-1641, 1981.
120. Watson, DeLamar M.; Hardy, Gordon H.; and Warner, David N., Jr.: Flight Test of the Glide-Slope Track and Flare-Control Laws for an Automatic Landing System for a Powered-Lift STOL Airplane. NASA TP-2128, 1983.
121. Meyer, George; and Cicolani, Luigi S.: Application of Nonlinear Systems Inverses to Automatic Flight Control Design: Systems Concepts and Flight Evaluations. In: AGARDograph 10, July 1981.
122. Cochrane, John A.; Riddle, Dennis W.; Stevens, Victor C.; and Shovlin, Michael D.: Selected Results from the Quiet Short-Haul Research Aircraft Flight Research Program. Journal of Aircraft, vol. 19, no. 12, Dec. 1982, pp. 1076-1082.
123. Stevens, Victor C.; Riddle, Dennis W.; Martin, James L.; and Innis, Robert C.: Powered-Lift STOL Aircraft Shipboard Operations: A Comparison of Simulation, Land-Based and Sea-Trials Results for the QSRA. AIAA Paper 81-2480, 1981.
124. Riddle, Dennis W.; Innis, Robert C.; Martin, James L.; and Cochrane, John A.: Powered-Lift Takeoff Performance Characteristics Determined from Flight Test of the Quiet Short-Haul Research Aircraft (QSRA). AIAA Paper 81-2409, Nov. 1981.
125. Stephenson, Jack D.; and Hardy, Gordon H.: Longitudinal Stability and Control Characteristics of the Quiet Short-Haul Research Aircraft (QSRA). NASA TP-2965, 1989.
126. Stephenson, Jack D.; Jeske, James A.; and Hardy, Gordon H.: Lateral- Directional Stability and Control Characteristics of the Quiet Short-Haul Research Aircraft (QSRA). NASA TM-102250, 1990.
127. Franklin, James A.; Hynes, Charles S.; Hardy, Gordon H.; Martin, James L.; and Innis, Robert C.: Flight Evaluation of Augmented Controls for Approach and Landing of Powered-Lift Aircraft. Journal of Guidance, Control, and Dynamics, vol. 9, no. 5, Sept.-Oct. 1986, pp. 555-565.
128. Hynes, Charles S.; Franklin, James A.; Hardy, Gordon H.; Martin, James L.; and Innis, Robert C.: Flight Evaluation of Pursuit Displays for Precision Approach of Powered-Lift Aircraft. Journal of Guidance, Control, and Dynamics, vol. 12, no. 4, July-Aug. 1989, pp. 521-529.
129. Hynes, Charles S.; Hardy, Gordon H.; and Kaisersatt, Thomas J.: Flight Evaluation of an Integrated Control and Display System for Precision Manual Landing Flare of Powered-Lift STOL Aircraft. SAE Proceedings of the 1987 International Powered Lift Conference, Paper P-203, Dec. 1987, pp. 165-180.
130. Watson, DeLamar M.; Hardy, Gordon H.; Innis, Robert C.; and Martin, James L.: Flight Evaluation of a Precision Landing Task for a Powered-Lift STOL Aircraft. AIAA-86-2130, Aug. 1986.
131. Cochrane, John A.; Riddle, Dennis W.; and Stevens, Victor C.: Quiet Short-Haul Research Aircraft: The First Three Years of Flight Research. AIAA-81-2625, Dec. 1981.
132. Riddle, Dennis W.; Stevens, Victor C.; and Eppel, Joseph C.: Quiet Short-Haul Research Aircraft: A Summary of Flight Research Since 1981. SAE Technical Paper 872315, Dec. 1987.
133. Anderson, Seth B.: Handling Qualities Criteria for V/STOL Aircraft. AGARDograph 46, pt. 2, June 1960, pp. 511-531.
134. Drinkwater, Fred J., III: Operational Technique for Transition of Several Types of V/STOL Aircraft. NASA TN D-774, 1961.
135. Turner, Howard L.; and Drinkwater, Fred J., III: Some Flight Characteristics of a Deflected Slipstream V/STOL Aircraft. NASA TN D-1891, 1963.
136. Pauli, Frank A.; Hegarty, Daniel M.; and Walsh, Thomas M.: A System for Varying the Stability and Control of a Deflected-Jet Fixed-Wing VTOL Aircraft. NASA TN D-2700, 1965.
137. Rolls, L. Stewart; and Drinkwater, Fred J., III: A Flight Determination of the Attitude Control Power and Damping Requirements for a Visual Hovering Task in the Variable Stability and Control X-14A Research Vehicle. NASA TN D-1328, 1962.
138. Rolls, L. Stewart; Drinkwater, Fred J., III; and Innis, Robert C.: Effects of Lateral Control Characteristics on Hovering a Jet Lift VTOL Aircraft. NASA TN D-2701, 1965.
139. Gerdes, Ronald M.; and Weick, Richard F.: A Preliminary Piloted Simulator and Flight Study of Height Control Requirements for VTOL Aircraft. NASA TN D-1201, 1962.
140. Feistel, Terrell W.; Gerdes, Ronald M.; and Fry, Emmett B.: An Investigation of a Direct Side-Force Maneuvering System on a Deflected Jet VTOL Aircraft. NASA TN D-5175, 1969.
141. Corliss, Lloyd D.; Greif, Richard K.; and Gerdes, Ronald M.: Comparison of Ground-Based and In-Flight Simulation of VTOL Hover Control Concepts. Journal of Guidance and Control, vol. 1, no. 3, May-June 1978, pp. 217-221.
142. Holzhauser, Curt A.; Morello, Samuel A.; Innis, Robert C.; and Patton, James M., Jr.: A Flight Evaluation of a VTOL Jet Transport Under Visual and Simulated Instrument Conditions. NASA TN D-6754, 1972.
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