[169] 1.1. Hansen, James R.: Engineer in Charge: A History of the Langley Aeronautical Laboratory, 1917-1958. NASA SP-4305, 1987.

 

2.1. Phillips, Hewitt: What Can Be Learned From Paper Airplanes. Soar Tech J. Radio Control. Soaring, no. 9, p. 109, Nov. 1992.

 

2.2. Phillips, Hewitt: History of the Jordan-Traveler Junior Aviation League. Twenty-Second Annual Report of the National Free Flight Society Symposium. George Xenakis, ed., 1989, pp. 68-72.

 

2.3. Phillips, Hewitt: Building a Wind Tunnel-An Educational Experience. Nineteenth Annual Symposium of the National Free Flight Society, 1986, pp. 73-79.

 

2.4. Phillips, William H.; and Levy, Charles N.: Effect of Pressure Gradients on the Boundary Layer Along a Flat Plate. Thesis, Massachusetts Institute of Technology, 1939.

 

2.5. Phillips, W. H.: Effect of Structural Flexibility on the Design of Vibration-lsolating Mounts for Aircraft Engines. NASA TM-85725, 1984.

 

2.6. Phillips, W. H.; and Rauscher, Manfred: Propulsive Effects of Radiator and Exhaust Ducting. J. Aeronaut. Sci., vol. 8, no. 4, Feb. 1941, pp. 167-174.

 

2.7. Phillips, Hewitt; and Tyler, Bill: Cutting Down the Drag. Twenty-Seventh Annual Symposium of the National Free Flight Society, 1994, pp. 14-18.

 

3.1. Phillips, William H.: Recollections of the Langley Memorial Aero Lab in the Forties. A.A.H.S. J., vol. 37, no. 2,1992, pp. 116-127.

 

4.1. Bryan, G. H.: Stability in aviation. MacMillan, 1911.

 

4.2. Soulé, H. A.: Preliminary Investigation of the Flying Qualities of Airplanes. NACA TR-700, 1940.

 

4.3. Gilruth, R. R.: Requirements for Satisfactory Flying Qualities of Airplanes. NACA Rep. 755, 1943. (Supersedes NACA ARC, Apr. 1941.)

 

4.4. 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 1941.

 

[170] 4.5. Nissen, J. M.; and Phillips, W. H.: Measurements of the Flying Qualities of a Hawker Hurricane Airplane. NACA WR L-565. Apr. 1942. (Formerly NACA MR, Apr. 1942.)

 

4.6. Phillips, W. H.: Flying Qualities From Early Airplanes to the Space Shuttle. AIAA J. Guid, Control, & Dyn., vol. 12, no. 4, 1989, pp. 449-459.

 

4.7. Phillips, William H.: A Flight Investigation of Short-Period Longitudinal Oscillations of an Airplane With Free Elevator. NACA WR L-444, 1942. (Formerly NACA ARR, May 1942.)

 

4.8Kleckner, Harold F.: Flight Tests of an All-Movable Vertical Tail on the Fairchild XR2K- I Airplane. NACA ACR No. 3F26, 1943.

 

4.9. Phillips, W. H.; Crane, H. L.; and Hunter, P. A.: Effect of Lateral Shift of Center of Gravity on Rudder Deflection Required for Trim. NACA WR L-92, 1944. (Formerly NACA RB L4I06.)

 

4.10. Phillips, William H.: Appreciation and Prediction of Flying Qualities. NACA Rep. 927, 1949. (Supersedes NACA TN 1670.)

 

4.11. Gilruth, R. R.; and White, M. D.: Analysis and Prediction of Longitudinal Stability of Airplanes. NACA Rep. 711, 1941.

 

5.1. Bode, Hendrik Wade: Network Analysis and Feedback Amplifier Design. D. Van Nostrand Co., Inc., 1945.

 

5.2. Bush, Vannevar: Operational Circuit Analysis. John Wiley & Sons, Inc., 1937.

 

5.3. Jones, R. T.: A Simplified Application of the Method of Operators to the Calculation of Disturbed Motions of an Airplane. NACA-TR-560, Jan. 1937.

 

5.4. Gardner, Murray F. and Barnes, John L.: Transients in Linear Systems Studied by the Laplace Transformation. Lumped-Constant Systems, Volume I, John Wiley &: Sons, Inc., 1942.

 

5.5. Minorsky, Nicolai: Introduction to Non-Linear Mechanics-Topological Methods, Analytical Methods, Non-Linear Resonance, Relaxation Oscillations. Ann Arbor: J. W. Edwards, 1947.

 

5.6. Weiss, Herbert K.: Dynamics of Constant-Speed Propellers. J. Aeron. Sci., vol. 70, pp. 58-67, Feb. 1943.

 

5.7. Lin, Shih-Nge: A Mathematical Study of the Controlled Motion of Airplanes. Thesis, Volume 1, Massachusetts Inst. of Technology, 1939.

 

5.8. Mueller, R. K.: The Graphical Solution of Stability Problems. J. Aeronaut. Sci., vol. 4, no. 8, June 1937, pp. 324 331.

 

5.9. Breuhaus, Waldemar O.: Resumé of the Time Vector Method as a Means for Analyzing Aircraft Stability Problems. WADC Tech. Rep. 52-299, U.S. Air Force, Nov. 1952.

 

5.10. Larrabee, E. E.: Application of the Time Vector Method to the Analysis of Flight Test Lateral Oscillation Data. C.A.L. FRM No. 189, Sept 1953.

 

5.11. Klawans, Bernard B.: A Simple Method for Calculating the Characteristics of the Dutch Roll Motion of an Airplane. NACA TN 3754, 1956.

 

6.1. Phillips, William H.: Application of Spring Tabs to Elevator Controls. NACA Rep. 797, 1944. (Formerly included in NACA ARR L4H28 and NACA RB L5A13.)

 

[171] 6.2. Phillips, William H.; and Thompson, Robert F.: Investigation by the Transonic-Bump Method of a 35 Degree Sweptback Semispan Model Equipped With a Flap Operated by a Series of Servovanes Located Ahead of and Geared to the Flap. NACA TN 3689, 1956.

 

7.1. Phillips, William H.: Preliminary Measurements of Flying Qualities of the Japanese Mitsubishi 00 Pursuit Airplane (U.S. Navy Designation Zero-2). NACA Mr. Bu. Aero, May 1943.

 

8.1. Phillips, William H.; and Cheatham, Donald C.: Ability of Pilots to Control Simulated Short-Period Yawing Oscillations. NACA RM L50D06, 1950.

 

8.2. Phillips, William H.: Effect of Steady Rolling on Longitudinal and Directional Stability. NACA TN 1627, 1948.

 

8.3. Sternfield, Leonard: Effect of Product of Inertia on Lateral Stability. NACA TN 1193, 1947.

 

8.4. Boucher, Robert W.; Rich, Drexel A.; Crane, Harold L.; and Matheny, Cloyce E.: A Method for Measuring the Product in Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane. NACA TN 3084, 1954.

 

8.5. Phillips, W. H.: Stability of a Body Stabilized by Fins and Suspended From an Airplane. NACA WR L-28, 1944. (Formerly NACA ARRL4D18.)

 

8.6. Rayleigh, John William Strutt, (Lord): The Theory of Sound. Dover Publ., 1945.

 

8.7. Phillips, William H.: Theoretical Analysis of Oscillations of a Towed Cable. NACA TN 1796, 1949.

 

8.8. Billing, Heinz: Oscillations excited in the cable of a bomb towed behind an aircraft. Tech. Trans, TT-88. Nat. Research Council of Canada, May 3,1949.

 

9.1. Theodorsen, Theodore: General Theory of Aerodynamic Instability and the Mechanism of Flutter. NACA Rep. 496, 1935.

 

9.2. Birnbaum, W.: The Uniplanar Problem of the Flapping Wing. Z.f a.MM, vol. 4, no. 4 Aug. 1924, pp. 277-292.

 

9.3. Wagner, Herbert: Uber die Entstehung des dynamischen Auftriebes von Tragflugeln. (The Origin of Dynamic Lift on Airplane Wings.) Z.f a.M.M., Bd. 5, Heft 1, Feb. 1925, pp. 17-35.

 

9.4. Glauert, H.: Force and Moment on an Oscillating Aerofoil. British R&M 1242, 1929.

 

9.5. Walker, P. B.: Growth of Circulation About a Wing and an Apparatus for Measuring Fluid Motion. British R&M 1402, 1931.

 

9.6. Smilg, Benjamin: The Instability of Pitching Oscillations of an Airfoil in Subsonic Incompressible Potential Flow. J. Aeronaut. Sci., vol. 16, no. 11, Nov. 1949, pp. 691-696.

 

9.7. Pinsker, W. J. G.: Note on the Dynamic Stability of Aircraft at High-Subsonic Speeds When Considering Unsteady Flow. ARC R&M 2904, 1950.

 

9.8. Jones, Robert T.: The Unsteady Lift of a Wing of Finite Aspect Ratio. NACA Rep. 681, 1940.

 

[172] 10.1. Phillips, William H.; Kuchnel, Helmut A.; and Whitten, James B.: Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes. NACA Rep. 1304, 1957. (Supersedes NACA TN 3637.)

 

11.1. 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 TN 4064, 1957.

 

11.2. McRuer, Duane: Human Dynamics and Pilot-lnduced Oscillations. Twenty-Second Minta Martin Lecture, MIT Dept. of Aeronautics and Astronautics, Dec. 2, 1992.

 

11.3. Koppen, O. C.: Airplane Stability and Control from a Designer's Point of View. J. Aeronautical Sciences, Feb. 1940, pp. 135-140.

 

11.4. Weiss, Herbert K.: Theory of Automatic Control of Airplanes. NACA TN 700, 1939.

 

11.5. Tustin, A.: The Nature of the Operator's Response in Manual Control and Its Implications for Controller Design. J. Inst. Electr. Eng., vol. 94, pt. IIA, no. 2, 1947, pp. 190-202.

 

11.6. Gustafson, F. B.; and O'Sullivan, William J., Jr.: The Effect of High Wing Loading on Landing Technique and Distance, With Experimental Data for the B-26 Airplane. NACA WR L-160, 1945. (Formerly NACA ARR L4K07, Jan. 1945.)

 

11.7. Von Doenhoff, Albert E.; and Jones, George W., Jr.: An Analysis of the Power-Off Landing Maneuver in Terms of the Capabilities of the Pilot and the Aerodynamic Characteristics of the Airplane. NACA TN 2967, 1953.

 

11.8. Von Doenhoff, Albert E.; and Hallissy, Joseph M., Jr.: Systems Using Solar Energy for Auxiliary Space Vehicle Power. Rep. No. 59-40, Inst. Aeronaut. Sci., Jan. 1959.

 

12.1. Einstein, A.: On the Movement of Small Particles Suspended in Stationary Liquids Required by the Molecular-Kinetic Theory of Heat. Annalen der Physik, vol. 17, 1905, pp. 549-560.

 

12.2. Taylor, G. I.: The Statistical Theory of Isotrophic Turbulence. J. of Aero. Sci., vol. 4, no. 8, Jun. 1937, pp. 311-314.

 

12.3. von Karman, T.: The Fundamentals of the Statistical Theory of Turbulence. J. of Aero. Sci., vol. 4, no. 4, Feb. 1937, p. 135.

 

12.4. Heisenberg, W.: On the Statistical Theory of Turbulence. Trans. of Zur Statistischen Theorie der Turbulnez. Zeitschrift fur Physik, vol. 124, 1948. NACA TM 1431, 1958.

 

12.5. Crane, Harold L.; and Chilton, Robert G.: Measurements of Atmospheric Turbulence Over a Wide Range of Wavelength for One Meteorological Condition. NACA TN 3702, 1956.

 

13.1. Hirsch, Rene: Recherches théoriques et expérimentales sur les moyens de soustraire un avion aux accélérations que peuvent engendrer les perturbations atmosphériques. Publ. No. 138, Publ. Sci. et Tech. du Ministère de l'Air (Paris), 1938.

 

13.2. Phillips, William H.; and Kraft, Christopher C., Jr.: Theoretical Study of Some Methods for lncreasing the Smoothness of Flight Through Rough Air. NACA TN 2416, 1951.

 

[173] 13.3. Cowley, W.L. and Glauert, H.: The Effect of the Lag of the Downwash on the Longitudinal Stability of an Aeroplane and on the Rotary Derivative. Mq. R. & M. No, 718, British A.R.C., 1921.

 

13.4. Kraft, Christopher C., Jr.: Initial Results of a Flight Investigation of a Gust-Alleviation System. NACA TN 3612, 1956.

 

13.5. Hunter, Paul A.; Kraft, Christopher C., Jr.; and Alford, William L.: A Flight Investigation of an Automatic Gust-Alleviation System in a Transport Airplane. NASA TN D-532, 1961.

 

13.6. Cooney, T. V.; and Schott, Russell L.: Initial Results of a Flight investigation of the Wing and Tail Loads on an Airplane Equipped With a Vane Controlled Gust-Alleviation System. NACA TN 3746, 1956.

 

13.7. Schott, Russell L.; and Hamer, Harold A.: Flight Investigation of Some Effects of a Vane-Controlled Gust-Alleviation System on the Wing and Tail Loads of a Transport Airplane. NASA TN D-643, 1961.

 

13.8. Barker, L. Keith; and Sparrow, Gene W.: Analysis of Effects of Spanwise Variations of Gust Velocity on a Vane-Controlled Gust-Alleviation System. NASA TN D-6126, 1971.

 

13.9. Barker, L. Keith: Effects of Spanwise Variation of Gust Velocity on Alleviation System Designed for Uniform Gust Velocity Across Span. NASA TN D-6346, 1971.

 

13.10. Phillips, William H.: Gust Alleviation. Performance and Dynamics of Aerospace Vehicles, NASA SP-258, 1971.

 

13.11. Hirsch, Rene: Etudes et Essais d'un Avion Absorbeur de Rafales. Docaéro, no. 42, Jan. 1957.

 

13.12. Hirsh, R.: L'Absorption des Rafales sur Avions et Resultats des Essais en Vol d'un Appareil Experimental. Doc-Air-Espace, no. 105, July 1967, pp. 41-56.

 

13.13. Burris, P. M.; and Bender, M. A.: Aircraft Load Alleviation and Mode Stabilization (LAMS). AFFDL-TR-68-158, U.S. Air Force, Apr. 1969.

 

13.14. Rynaski, E. G.; Andrisani, D., II; and Weingarten, N.: Active Control for the Total-ln Flight Simulator (ACTIFS). NASA CR-3118, 1979.

 

14.1. Ribner, H. S.: Spectral Theory of Buffeting and Gust Response: Unification and Extension. J. Aeronautical Sciences, vol. 23, no. 12, Dec. 1956.

 

14.2. Etkin, Bernard: Dynamics of Flight. John Wiley & Sons, 1959.

 

14.3. Diederich, Franklin W.: The Response of an Airplane to Random Atmospheric Disturbances. NACA Rep. 1345, 1958.

 

14.4. Eggleston, John M.; and Diederich, Franklin W.: Theoretical Calculation of the Power Spectra of the Rolling and Yawing Moments on a Wing in Random Turbulence. NACA Rep. 1321, 1957. (Supersedes NACA TN 3864.)

 

14.5. Eggleston, John M.; and Phillips, William H.: The Lateral Response of Airplanes to Random Atmospheric Turbulence. NASA TR R-74, 1960. (Supersedes NACA TN 3954 by Eggleston and TN 4196 by Eggleston and Phillips.)

 

14.6. Eggleston, John M.; and Phillips, William H.: A Method for the Calculation of the Lateral Response of Airplanes to Random Turbulence. NACA TN 4196, 1958.

[174] 15.1. National Safety Board Report. Aviat. Week & Space Technol., 1968.Part I-Turbulence Cited in BAC 111 Crash, June 10, 1968. Part 2-Low-Level Turbulence Study Urged. June 17, 1968.

15.2. Duncan, W. J.: The Representation of Aircraft Wings, Tails and Fuselages by Semi-Rigid Structures in Dynamic and Static Problems. British R&M 1904, 1943.

 

15.3. Adams, James J.; and Whitten, James B.: Flying Qualities of a High-Performance Personal-Owner Airplane. NACA RM SLSlF18, CAA, 1951.

 

15.4. U.S. Dept. of Transportation, Transportation Systems Center: Task Force Report, V-Tail Bonanza Investigation. Prepared for the FAA, Jan. 1986.

 

16.1. Phillips, William H., compl.: NACA Flight Research on the Vought F8U-I Airplane, Dec. 1981. (Available from NASA Langley Research Center, Hampton, VA.)

 

16.2. Kraft, Christopher C., Jr.; McLaughlin, Milton D.; White, Jack A.; and Champine, Robert A.: Flight Measurements of Some of the Flying Qualities and Stability Derivatives of a Supersonic Fighter Airplane. NASA Memo Rep. 10-7-58L, 1958.

 

18.1. Katzoff, S.: Clarity in Technical Reporting. NASA SP-7010, 1964.

 

19.1. Hansen, James R.: Spaceflight Revolution-NASA Langley Research Center From Sputnik to Apollo. NASA SP-4308, 1995.

 

19.2. Morin, Relman: Expert Says Sputnik Won The Cold War. Newport News (VA) Daily Press, Jan. 7, 1958, p. 1.

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