[181] NACA or NASA Reports
1. Phillips, William H.; and Vensel, J. R.: Measurements of the Flying Qualities of a Curtiss P-40 Airplane (AC No. 39-160). NACA CMR, Army Air Corps, May 31, 1941.
2. Phillips, William H.; and Gough, Melvin N.: Investigation of Aileron Characteristics of the Vought-Sikorsky XF4U-1 Airplane. Memorandum Report for Navy, Aug. 15, 1941.
3. Phillips, William H.; and Gough, Melvin N.: Measurements of the Longitudinal Stability and Control Characteristics of the Vought-Sikorsky XF4U- 1 Airplane. Memorandum Report for Navy, Aug. 30, 1941.
4. Phillips, William H.: Effect of Spring and Gravity Moments in the Control System on the Longitudinal Stability of the Brewster XSBA- 1 Airplane. NACA ARR, Apr. 1942. (Wartime Report L-263.)
5. Phillips, William H.; and Nissen, J. M.: Measurements of the Flying Qualities of a Hawker Hurricane Airplane. NACA MR for AAF, Apr. 20, 1942. (Wartime Report L-565.)
6. Phillips, William H.: A Flight Investigation of Short Period Longitudinal Oscillations of an Airplane with Free Elevator. NACA ARR, May 1942. (Wartime Report L-444.)
7. Phillips, William H.: Control-Surface Instability on High Speed Airplanes. NACA CB, June 1942.
8. Phillips, William H.: Comparison of Aileron Control Characteristics as Determined in Flight Tests of P-36, P-40, Spitfire, and Hurricane Pursuit Airplanes. NACA CB, Aug. 1942.
9. Phillips, William H.; and Vensel, J. R.: Measurements of the Flying Qualities of the Supermarine Spitfire VA Airplane. NACA ACR, Sept. 1942. (Wartime Report L-334.)
10. Phillips, William H.; and Vensel, J. R.: Stalling Characteristics of the Supermarine Spitfire VA Airplane. NACA ACR, Sept. 1942. (Wartime Report L-353.)
11. Phillips, William H.: Preliminary Measurements of Flying Qualities of the Japanese Mitsubishi 00 Pursuit Airplane. (US Navy Designation Zero-2) NACA MR Bu. Aero. May 5, 1943.
[182] 12. Phillips, William H.; and Nissen, J. M.: Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane. I-Measurements of Flying Qualities with Original Tail Surfaces. NACA ARR 3F07, June 1943. (Wartime Report L-612.)
13. Phillips, William H.; and Crane, Harold L.: Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane. II-Measurements of Flying Qualities with Tail Configuration Number Two. NACA MR, Dec. 1943. (Wartime Report L-589.)
14. Phillips, William H.: Stability of a Body Stabilized by Fins and Suspended From an Airplane. NACA ARR L4D12, Apr. 1944. (Wartime Report L-28.)
15. Phillips, William H.; Williams, W. C.; and Hoover, H. H.: Measurements of Flying Qualities of a Curtiss SB2C-1 Airplane (No. 000 14). NACA MR, Bu. Aero. Mar. 14, 1944. (Wartime Report L-571.)
16. Phillips, William H.: Application of Spring Tabs to Elevator Controls. NACA ARR L8H28, Oct. 1944. (Wartime Report L- 122.)
17. Phillips, William H.; Crane, Harold L.; and Hunter, Paul A.: Effect of Lateral Shift of Center of Gravity on Rudder Deflection Required for Trim. NACA RB L4I06, Nov. 1944. (Wartime Report L-92.)
18. Phillips, William H.: Application of Spring Tabs to Elevator Controls. NACA Report No. 797, 1944.
19. Phillips, William H.: An Investigation of Additional Requirements for Satisfactory Elevator Control Characteristics. NACA MR LSG16, May 1945. (Republished as TN 1060, June 1946.)
20. Phillips, William H.: The Use of Geared Spring Tabs for Elevator Control. NACA RB LSA13, Feb. 1945. (Wartime L-30.)
21. Phillips, William H.: Effect of Steady Rolling on Longitudinal and Directional Stability. NACA 1627, June 1948.
22. Phillips, William H.: Appreciation and Prediction of Flying Qualities. NACA TN-1670, Aug. 1948. (Republished as NACA Report 927, 1949.)
23. Phillips, William H.: Theoretical Analysis of Oscillations of a Towed Cable. NACA TN 1796, Nov. 1948.
24. Phillips, William H.; and Adams, J. J.: Low-Speed Tests of a Model Simulating the Phenomenon of Control-Surface Buzz. NACA RM LSOFI9, Aug. 1950.
25. Phillips, William H.; and Cheatham, Donald C.: Ability of Pilots to Control Simulated Short-Period Yawing Oscillations. NACA RM LSOD06, Nov. 1950.
26. Phillips, William.; and Kraft, C. C., Jr.: Theoretical Study of Some Methods for Increasing the Smoothness of Flight Through Rough Air. NACA TN 2416, July 1951.
27. Phillips, William, H.; and Thompson, R. F.: Investigation by the Transonic-Bump Method of a 35° Semispan Model Equipped With a Flap Operated by a Series of Servo-Vanes Located Ahead of and Geared to the Flap. NACA RM LSIJ10, Dec. 1951. (Republished as TN 3689, Apr. 1956.)
28. Phillips, William H.: Theoretical Analysis of Some Simple Types of Acceleration Restrictors. NACA TN 2574, Dec. 1951.
[183] 29. Phillips, William H.; Brown, B. Porter; and Matthews, James T., Jr.: Review and Investigation of Unsatisfactory Control Characteristics Involving Instability of Pilot-Airplane Combination and Methods for Predicting These Difficulties From Ground Tests. NACA RM L53F17a, Aug. 1953. (Republished as TN 4064, Aug. 1957.)
30. Phillips, William H.: Graphical Solution of Some Automatic-Control Problems Involving Saturation Effects With Application to Yaw Dampers for Aircraft. NACA TN 3034, Oct. 1953.
31. Phillips, W. H.; and Kuehnel, H. A.: Theoretical Investigation of Some Discontinuous Yaw Dampers. NACA RM L54B24a, Apr. 1954.
32. Phillips, W. H.: Investigation of Effect of Reduction of Valve Friction in a Power Control System by Use of a Vibrator. NACA RM LSSE18a, July 1955.
33. Phillips, W. H.; Kuchnel, H. A.; and Whitten, J. B.: Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device For Personal Airplanes. NACA TN 3637, Apr. 1956. (Changed to NACA Report 1304.)
34. Phillips, William H.: Analysis of an Automatic Control to Prevent Rolling Divergence. NACA RM L56A04, Apr. 1956.
35. Phillips, William H.: Loads Implication of Gust-Alleviation Systems. NACA TN 4056, June 1957.
36. Eggleston, John M.; and Phillips, William H.: The Lateral Response of Airplanes to Random Atmospheric Turbulence. TR R-74, 1960. (Supersedes TN-4196.)
37. Phillips, William H.: Analysis of Effects of Interceptor Roll Performance and Maneuverability on Success of Collision Course Attacks. NASA TN D-952, Aug. 1961. (Supersedes RM L-58E27.)
38. Phillips, William H.: Research on Blunt Faced Entry Configurations at Angles of Attack Between 60° and 90°. NASA TM X-315, Sept. 1960.
39. Phillips, William H.: NASA Reports-A Discussion for Prospective Authors. Jan. 3, 1962.
40. Phillips, W. H.; Queijo, M. J.; and Adams, James J.: Langley Research Center Simulation Facilities for Manned Space Missions. NASA TM X-50390, July 1965.
41. Phillips, William H.: Propulsive Efficiency of Tail-Mounted Turbofan Engines. NASA LWP-693, Dec. 17, 1968.
42. Phillips, William H.: Gust Alleviation. In: Performance and Dynamics of Aerospace Vehicles. NASA SP-258, 1971.
43. Phillips, William H.: Study of a Control System to Alleviate Aircraft Response to Horizontal and Vertical Gusts. NASA TN D-7278, Dec. 1973.
44. Phillips, William H.; and Lichtenstein, Jacob H.: Comparison of Effects of Unsteady Lift and Spanwise Averaging in Flight Through Turbulence. NASA TM X-74028, June 1977.
45. Phillips, William H.: Ground Distance Covered During Airborne Horizontal Deceleration of an Airplane. NASA TP- 1157, Apr. 1978.
46. Phillips, William H.: Simulation Study of the Oscillatory Longitudinal Motion of an Airplane at the Stall. NASA TP-1242, Aug. 1978.
[184] 47. Phillips, William H.: Altitude Response of Several Airplanes during Landing Approach. NASA TM-80186, Nov. 1979.
48. Some Design Considerations for Solar-Powered Aircraft. NASA TP- 1675, June 1980.
49. Phillips, William H.: Effect of Structural Flexibility on the Design of Vibration-Isolating Mounts for aircraft Engines. NASA TM-85725, Feb. 1984.
50. Phillips, William H.; and Grafton, Sue B.: Study of Canard Surfaces on the Shuttle Orbiter. NASA TM-89156, Sept. 1987.
51. Phillips, William H.: Determination of the Pressure Drag of Airfoils by Integration of Surface Pressures. NASA TM-102722, Oct. 1990.
Papers Other Than NACA or NASA Reports
1. Phillips, William H.; and Rauscher, M.: Propulsive Effects of Radiator and Exhaust Ducting. J. Aeronaut. Sci., vol. 8, no. 4, Feb. 1941, p.l67.
2. Phillips, William H.: Flying Qualities Requirements for Personal Airplanes. NACA- Industry Conference on Personal Aircraft Research, Sept. 1946.
3. Phillips, William H.: Low-Speed Flight Investigation of an Airplane with Sweptback Wings. NACA Conference on Aerodynamic Problems of Transonic Airplane Design, Nov. 1947, pp. 145-152.
4. Phillips, William H.: Flying and Handling Qualities of Airplanes. NACA-University Conference on Aerodynamics, June 1948.
5. Phillips, William H.: Flying Qualities of Airplanes at Transonic Speeds. Talk at Test Pilot Training School, NATC, Patuxent, June 2, 1949.
6. Phillips, William H.: Analysis of Means to Increase the Smoothness of Flight Through Rough Air. NACA Conference on Some Problems of Aircraft Operation, Oct. 1950.
7. Phillips, William H.: Power Control Systems, Artificial Feel, and Acceleration Restrictors. NACA Conference on High-Speed Airplane Aerodynamics, Dec. 1951.
8. Phillips, William H.: Recent Studies of Stability and Control Characteristics of Fighter Airplanes and Their Relation to Tactical Requirements. Talk at Test Pilot Training School, NATC. Patuxent, June 13, 1952.
9. Phillips, William H.: Stability and Control Problems at Transonic and Supersonic Speeds and Problems of Aiming and Sighting Guns at Transonic Speeds. Talk for Ad Hoc Group on Airborne Fire Control Systems for Fighter Aircraft, Research and Development Board, Dec. 11, 1952.
10. Phillips, William H.: High-Speed Stability and Control Problems. Presented to Flight Test Panel of the Advisory Group for Aeronautical Research and Development of NATO, May 1953.
11. Phillips, William H.: High-Speed Flight Stability and Control Problems. Talk at Test Pilot Training School, NATC, Patuxent, June 28, 1954.
[185] 12. Phillips, William H.: Power Control Systems and Control Feel Devices for Satisfactory Airplane Handling Qualities. NACA Conference on Some Problems of Aircraft Operation, Nov. 1954.
13. Phillips, William H.: A Study of Means of Limiting the Maximum Normal Acceleration of Airplanes. NACA Conference on Automatic Stability and Control of Aircraft, Mar. 1955.
14. Phillips, William H.; and Williams, W. C.: Some Recent Research on the Handling Qualities of Airplanes. NACA Conference on Aerodynamics of High-Speed Aircraft, Nov. 1955.
15. Phillips, William H.: Similarities and Contrasts Between Ship Design and Aircraft Design Stability and Control. Bull. Soc. Naval Arch. & Mar. Eng., vol. XI, no. 2, July 1956.
16. Phillips, William H.: Loads Implications of Gust-Alleviation Systems. NACA Conference on Aircraft Loads, Structures, and Flutter. Mar. 1957.
17. Phillips, William H.: High-Speed Stability and Control Problems. AGARD Flight Test Manual, Vol. II, Chapt. 9, Pt. I.
18. Phillips, William H.: Flight Measurements of the Stability and Controllability of Airplanes. Princeton Series, Volume VII-Experimental Methods in High-Speed Aerodynamics.
19. Phillips, William H.; Queijo, M. J.; end Adams, James J.: Langley Research Center Simulation Facilities for Manned Space Missions. Published in ASME Publication-Paper No. 63-AHGT-91. (Contributed by the Aviation and Space Division for Presentation at the Aviation and Space, Hydraulic, and Gas Turbine Conference and Products Show. Los Angeles, CA., Mar. 1963.
20. Phillips, William H.: Gust Alleviation. Lecture presented at Rensselaer Polytechnic Institute, Spring 1970.
21. Phillips, William H.: Analysis of Effect of Asymmetric Loading on Sailplane Performance in Circling Flight. Paper presented at the Symposium on the Technology and Science of Motorless Flight. Cambridge, Massachusetts (M.I.T.), Oct. 1972.
22. Phillips, William H.: Analysis and Experimental Studies of the Control of Hang Gliders. Presented at the AIAA/MIT/SSA Second International Symposium on the Technology and Science of Low-Speed and Motorless Flight, Cambridge, Massachusetts, Sept. 1974.
23. Phillips, William H.: Stability and Control of Hang Gliders. Presented at the Soc. of Auto. Eng. Meeting. Dayton, Ohio, Sept. 1976.
24. Phillips, William H.: Gyroscopic Moments on a Glider in Turing Flight. Technical Soaring, 1973.
25. Stewart, E. C.; Phillips, W. H.; and Hewes, D. E.: Gust Alleviation System to Improve the Ride Comfort of Light Airplanes. NACA Technology Utilization Program Report LAR-11711, Oct. 1975.
26. Phillips, William H.: Propulsive Effects Due to Flight Through Turbulence. Engineering Note Published in J. Aircr., vol. 12, no. 7, July 1975, pp. 624 626.
27. Phillips, W. H.: Recovery from a Vertical Dive. Ground Skimmer, No. 31, Aug. 1975, pp. 18-21.
28. Phillips, W. H.: More on Dive Recovery, or Lack Thereof. Ground Skimmer, No. 34, Nov. 1975, pp. 24-25.
[186] 29. Phillips, William H.; and Shaughnessy, John D.: Investigation of Longitudinal Control System for a Small Hydrofoil Boat. J. of Hydro., vol. 10, no. 2, Apr. 1976.
30. Phillips, W. H.: Building a Wind Tunnel-An Educational Experience. 19th Annual Symposium of National Free Flight Society, 1986, pp. 73-79.
31. Phillips, William H.: Propeller Design Program. NASA Technology Utilization Program Report. LAR-13141 and LAR-12142, vol. 8, no. 4, Apr. 1985.
32. Phillips, W. H.: Research on the Energy Efficiency of Fireplaces. Contract DE-FG43-81R308099, (Work conducted at VARC for DOE. Final Report), College of William and Mary, Virginia, Associated Research Center Campus, Oct. 1982.
33. Phillips, William H.: Flying Qualities from Early Airplanes to the Space Shuttle. J. Guid., Control, & Dyn., vol. 12, no. 4, July 1989, pp. 449-459.
34. Phillips, William H.: Studies of Friction Drag and Pressure Drag of Airfoils Using the Eppler Program. SAE TP-881396, Oct. 1988.
35. Phillips, William H.: Recollections of the Langley Memorial Aero Lab in the Forties. J. American Aviat. Hist. Soc., vol. 37, no. 2, Summer 1992, pp. 116-127.
36. Phillips, W. H.: Effects of Model Scale on Flight Characteristics and Design Parameters. AIAA J. Aircr., vol. 31, no. 2, Mar. 1994, pp. 454 457.
Unpublished Papers in NASA Langley Research Center Library
1. Phillips, William H.: Dynamic Longitudinal Stability of Airplanes, L.A.L. Notes for Lectures Presented in UVA Extension Course, 1956. (Unpublished, Library No. *CN-47503.)
2. Phillips, W. H.: Correlation of Data Obtained by various test methods at Transonic Speeds. Oct. 7, 1946. (Unpublished, Library No. 1111262.)