Subject: NACA Publication
Number of records: 81.
Weil, Joseph and Day, Richard E. (1956) An Analog Study of the Relative Importance of Various Factors Affecting Roll Coupling. Technical Report NACA RM H56A06, Research Engineering, NASA Dryden Flight Research Center.
Marcy, William L. and Stephenson, Harriet J. and Cooney, Thomas V. (1956) Analysis of the Vertical-Tail Loads Measured During a Flight Investigation at Transonic Speeds of the Douglas X-3 Research Airplane. Technical Report NACA RM H56H08, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Stillwell, Wendell H. (1955) Behavior of the Bell X-1A Research Airplane During Exploratory Flights at Mach Numbers Near 2.0 and at Extreme Altitudes. Technical Report NACA RM H55G25, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. and Drake, Hubert M. and Fischel, Jack (1956) Comparison of Flight and Wind-Tunnel Measurements of High-Speed-Airplane Stability and Control Characteristics. Technical Report NACA TN 3859, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Day, Richard E. (1956) Correlation of Flight and Analog Investigations of Roll Coupling. Technical Report NACA RM H56F08, Research Engineering, NASA Dryden Flight Research Center.
Angle, Ellwyn E. and Holleman, Euclid C. (1950) Determination of Longitudinal Stability of the Bell X-1 Airplane from Transient Responses at Mach Numbers up to 1.12 at Lift Coefficients of 0.3 and 0.6. Technical Report NACA RM L50I06a, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1957) Dynamic Longitudinal Stability Characteristics of a Swept-Wing Fighter-Type Airplane at Mach Numbers Between 0.36 and 1.45. Technical Report NACA RM H56H03, Research Engineering, NASA Dryden Flight Research Center.
Matthews Jr., James T. (1948) Effect of Downwash on the Estimated Elevator Deflection Required for Trim of the XS-1 Airplane at Supersonic Speeds. Technical Report NACA RM L8H06a, Research Engineering, NASA Dryden Flight Research Center.
Fischel, Jack and Reisert, Donald (1955) Effect of Several Wing Modifications on the Low-Speed Stalling Characteristics of the Douglas D-558-II Research Airplane. Technical Report NACA RM H55E31a, Research Engineering, NASA Dryden Flight Research Center.
Fischel, Jack and Reisert, Donald (1956) Effect of Several Wing Modifications on the Subsonic and Transonic Longitudinal Handling Qualities of the Douglas D-558-II Research Airplane. Technical Report NACA RM H56C30, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1950) Effects on the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane. Technical Report NACA RM L50I05, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Clagett, Harry P. (1951) Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder. Technical Report NACA RM L50K01a, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Carden, John R. (1950) Elevator-Stabilizer Effectiveness and Trim of the X-1 Airplane to a Mach Number of 1.06. Technical Report NACA RM L50G20, Research Engineering, NASA Dryden Flight Research Center.
Thompson, Jim Rogers and Bray, Richard S. and Cooper, George E. (1955) Flight Calibration of Four Airspeed Systems on a Swept-Wing Airplane at Mach Numbers up to 1.04 by the NACA Radar-Phototheodolite Method. Technical Report NACA TN 3526, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. and Walker, Joseph A. (1956) Flight Determination of the Lateral Handling Qualities of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H56C29, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. (1955) Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H55C07, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Andrews, William H. and Darville, Robert W. (1957) Flight Evaluation of the Lateral Stability and Control Characteristics of the Convair YF-102 Airplane. Technical Report NACA RM H56G11, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Gates Jr., Ordway B. and Banner, Richard D. and Kuhl, Albert E. (1955) Flight Experience of Inertia Coupling in Rolling Maneuvers. Technical Report NACA RM H55E17b, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Andrews, William H. (1955) Flight Experience with a Delta-Wing Airplane Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. Technical Report NACA RM H55H03, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1956) Flight Experience with Present Research Airplanes. Technical Report NACA-CONF-26-Oct-56-p15-22, Research Engineering, NASA Dryden Flight Research Center.
Staff, NACA (1955) Flight Experience with Two High-Speed Airplanes Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. Technical Report NACA RM H55A13, Research Engineering, NASA Dryden Flight Research Center.
Thompson, Jim Rogers and Roden, William S. and Eggelston, John M. (1950) Flight Investigation of the Aileron Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Between 0.6 and 0.89. Technical Report NACA RM L50D20, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. and Peele, James R. and Day, Richard E. (1956) Flight Investigation of the Effect of Vertical-Tail Size on the Rolling Behavior of a Swept-Wing Airplane Having Lateral-Longitudinal Coupling. Technical Report NACA RM H55L28a, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Finch, Thomas W. and Peele, James R. (1955) Flight Measurements of Directional Stability to a Mach Number of 1.48 for an Airplane Tested with Three Different Vertical Tail Configurations. Technical Report NACA RM H55G26, Research Engineering, NASA Dryden Flight Research Center.
Reed, Robert D. (1955) Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees. Technical Report NACA RM H55E20a, Research Engineering, NASA Dryden Flight Research Center.
Knapp, Ronald J. and Johnson, Wallace E. (1953) Flight Measurements of Pressures on Base and Rear Part of Fuselage of the Bell X-1 Research Airplane at Transonic Speeds, Including Power Effects. Technical Report NACA RM-L52L01, Research Engineering, NASA Dryden Flight Research Center.
Videan, Edward N. (1955) Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H55H10, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. (1955) Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55E26, Research Engineering, NASA Dryden Flight Research Center.
Carner, H. Arthur and Knapp, Ronald J. (1950) Flight Measurements of the Pressure Distribution on the Wing of the X-1 Airplane (10-Percent-Thick Wing) over a Chordwise Station near the Midspan, in Level Flight at Mach Numbers from 0.79 to 1.00 and in a Pull-Up at a Mach Number of 0.96. Technical Report NACA RM L50H04, Research Engineering, NASA Dryden Flight Research Center.
Childs, Joan M. (1953) Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Degrees Sweepback. Technical Report NACA RM-L52K13b, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Clinton T. (1955) Flight Measurements of the Vertical-Tail Loads on the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55H25, Research Engineering, NASA Dryden Flight Research Center.
Kuhl, Albert E. and Johnson, Clinton T. (1955) Flight Measurements of Wing Loads on the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55D12, Research Engineering, NASA Dryden Flight Research Center.
Mayer, John P. and Valentine, George M. (1951) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane – Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87. Technical Report NACA RM L50J13, Research Engineering, NASA Dryden Flight Research Center.
Wilmerding, J. V. and Stillwell, W. H. and Sjoberg, S. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Lateral Control Characteristics as Measured in Abrupt Aileron Rolls at Mach Numbers up to 0.86. Technical Report NACA RM L50E17, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, W. H. and Wilmerding, J. V. and Champine, R. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Low-Speed Stalling and Lift Characteristics. Technical Report NACA RM L50G10, Research Engineering, NASA Dryden Flight Research Center.
Sjoberg, S. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers up to 0.87. Technical Report NACA RM L50C14, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and Bellman, Donald R. and Saltzman, Edwin J. (1956) Flight Techniques for Determining Airplane Drag at High Mach Numbers. Technical Report NACA TN 3821, Research Engineering, NASA Dryden Flight Research Center.
Jordan, Gareth H. and Keener, Earl R. (1955) Flight-Determined Pressure Distributions Over a Section of the 35 Degree Swept Wing of the Douglas D-558-II Research Airplane at Mach Numbers up to 2.0. Technical Report NACA RM H55A03, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Bellman, Donald R. and Musialowski, Norman T. (1956) Flight-Determined Transonic Lift and Drag Characteristics of the YF-102 Airplane with Two Wing Configurations. Technical Report NACA RM H56E08, Research Engineering, NASA Dryden Flight Research Center.
Dryden, Dr. Hugh L. (1956) General Background of the X-15 Research-Airplane Project. Technical Report NACA-CONF-26-Oct-56-pxvii-xxi, Research Engineering, NASA Dryden Flight Research Center.
Taback, I. and Truszynski, G. M. (1956) Instrumentation for the X-15. Technical Report NACA-CONF-26-Oct-56-p183-191, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Muhleman, Duane O. (1955) Lateral Stability and Control Characteristics of the Convair XF-92A Delta-Wing Airplane as Measured in Flight. Technical Report NACA RM H55A17, Research Engineering, NASA Dryden Flight Research Center.
Nugent, Jack (1956) Lift and Drag of the Bell X-5 Research Airplane in the 45 Degree Sweptback Configuration at Transonic Speeds. Technical Report NACA RM H56E02, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1948) Limited Measurements of Static Longitudinal Stability in Flight of Douglas D-558-I Airplane. Technical Report NACA RM L8E14, Research Engineering, NASA Dryden Flight Research Center.
Andrews, William H. and Sisk, Thomas R. and Darville, Robert W. (1956) Longitudinal Stability Characteristics of the Convair YF-102 Airplane Determined from Flight Tests. Technical Report NACA RM H56I17, Research Engineering, NASA Dryden Flight Research Center.
Sadoff, Melvin and Sisk, Thomas R. (1950) Longitudinal-Stability Characteristics of the Northrop X-4 Airplane (USAF No. 46-677). Technical Report NACA RM A50D27, Research Engineering, NASA Dryden Flight Research Center.
Brunn, Cyril D. and Stillwell, Wendell H. (1956) Mach Number Measurements and Calibrations During Flight at High Speeds and at High Altitudes Including Data for the D-558-II Research Airplane. Technical Report NACA RM H55J18, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1949) Measured Characteristics of the Douglas D-558-I Airplane (BuAero No. 37971) in Two Landings. Technical Report NACA RM L9D20a, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1949) Measurements of Aileron Effectiveness of the Bell X-1 Airplane at Mach Numbers Between 0.9 and 1.06. Technical Report NACA RM L9G19a, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and McLaughlin, Milton D. and Clift, Dorothy C. (1948) Measurements of the Chordwise Pressure Distributions Over the Wing of the XS-1 Research Airplane in Flight. Technical Report NACA RM L8G21, Research Engineering, NASA Dryden Flight Research Center.
Jordan, Gareth H. and Hutchins Jr., C. Kenneth (1955) Preliminary Flight-Determined Pressure Distributions Over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers. Technical Report NACA RM H55A10, Research Engineering, NASA Dryden Flight Research Center.
Sjoberg, Sigurd A. (1949) Preliminary Measurements of the Dynamic Lateral Stability Characteristics of the Douglas D-558-II (BuAero No. 37974) Airplane. Technical Report NACA RM L9G18, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Goodman, Harold R. and Hoover, Herbert H. (1948) Preliminary Results of NACA Transonic Flights of the XS-1 Airplane with 10-Percent-Thick Wing and 8-Percent-Thick Horizontal Tail. Technical Report NACA RM L8I29, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. and Briggs, Donald W. (1953) Preliminary Results of Stability and Control Investigation of the Bell X-5 Research Airplane. Technical Report NACA RM-L52K18b, Research Engineering, NASA Dryden Flight Research Center.
McLaughlin, Milton D. and Clift, Dorothy C. (1948) Results Obtained During a Dive Recovery of the Bell XS-1 Airplane to High Lift Coefficients at a Mach Number Greater than 1.0. Technical Report NACA RM L8C23a, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and McLaughlin, Milton D. and Goodman, Harold R. (1948) Results Obtained During Accelerated Transonic Tests of the Bell XS-1 Airplane in Flights to a Mach Number of 0.92. Technical Report NACA RM L8A05a, Research Engineering, NASA Dryden Flight Research Center.
Goodman, Harold R. and Drake, Hubert M. (1948) Results Obtained During Extension of U.S. Air Force Transonic-Flight Tests of XS-1 Airplane. Technical Report NACA RM L8I28, Research Engineering, NASA Dryden Flight Research Center.
Matthews Jr., James T. (1950) Results Obtained During Flights 1 to 6 of the Northrop X-4 Airplane (A.F. No. 46-677). Technical Report NACA RM L9K22, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1949) Results Obtained from Second Flight of X-4 Airplane (A.F. No. 46-676). Technical Report NACA RM L9F21, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1949) Results Obtained from Third Flight of Northrop X-4 Airplane (A.F. 46-676). Technical Report NACA RM L9G20a, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. (1955) Results of Measurements Made During the Approach and Landing of Seven High-Speed Research Airplanes. Technical Report NACA RM H54K24, Research Engineering, NASA Dryden Flight Research Center.
Williams, W. C. and Beeler, De E. (1948) Results of Preliminary Flight Tests of the XS-1 Airplane (8-Percent Wing) to a Mach Number of 1.25. Technical Report NACA RM L8A23a, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. and Drake, Hubert M. (1958) Simulator Studies of Jet Reaction Controls For Use at High Altitude. Technical Report NACA RM H58G18A, Research Engineering, NASA Dryden Flight Research Center.
Banner, Richard D. and Malvestuto Jr., Frank S. (1956) Skin and Structural Temperature Measurements on Research Airplanes at Supersonic Speeds. Technical Report NACA-CONF-26-Oct-56-p101-112, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. and Drake, Hubert M. and Fischel, Jack (1956) Some Correlations of Flight-Measured and Wind-Tunnel Measured Stability and Control Characteristics of High-Speed Airplanes. Technical Report NACA H56AG62, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. and Phillips, William H. (1956) Some Recent Research on the Handling Qualities of Airplanes. Technical Report NACA RM H55L29a, Research Engineering, NASA Dryden Flight Research Center.
Day, Richard E. and Fischel, Jack (1955) Stability and Control Characteristics Obtained During Demonstration of the Douglas X-3 Research Airplane. Technical Report NACA RM H55E16, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1949) Stability and Control Data Obtained from First Flight of X-4 Airplane. Technical Report NACA RM L9A31, Research Engineering, NASA Dryden Flight Research Center.
Valentine, George M. (1949) Stability and Control Data Obtained from Fourth and Fifth Flights of the Northrop X-4 Airplane (A.F. No. 46-676). Technical Report NACA RM L9G25a, Research Engineering, NASA Dryden Flight Research Center.
Barlow, William H. and Lilly, Howard C. (1949) Stability Results Obtained with Douglas D-558-I Airplane (BuAero No. 37971) in Flight up to a Mach Number of 0.89. Technical Report NACA RM L8K03, Research Engineering, NASA Dryden Flight Research Center.
Sadoff, Melvin and Sisk, Thomas R. (1950) Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677). Technical Report NACA RM A50A04, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Stillwell, Wendell H. and Armistead, Katharine H. (1957) Static-Pressure Error Calibrations for Nose-Boom Airspeed Installations of 17 Airplanes. Technical Report NACA RM H57A02, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. (1956) Studies of Reaction Controls. Technical Report NACA-CONF-26-Oct-56-p175-181, Research Engineering, NASA Dryden Flight Research Center.
Sadoff, Melvin and Sisk, Thomas R. (1950) Summary Report of Results Obtained During Demonstration Tests of the Northrop X-4 Airplanes. Technical Report NACA RM A50I01, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Pierce, Mary (1950) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the Douglas D-558-I Airplane for a 1g Stall, a Speed Run to a Mach Number of 0.90, and a Wind-Up Turn at a Mach Number of 0.86. Technical Report NACA RM L50J10, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Peele, James R. and Woodbridge, Julia B. (1951) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the Douglas D-558-I Airplane Throughout the Normal-Force-Coefficient Range at Mach Numbers of 0.67, 0.74, 0.78, and 0.82. Technical Report NACA RM L50L12a, Research Engineering, NASA Dryden Flight Research Center.
Carner, H. Arthur and Payne, Mary M. (1950) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in Level Flight at Mach Numbers from 0.79 to 1.00 and in a Pull-Up at a Mach Number of 0.96. Technical Report NACA RM L50H25, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1956) Time-Vector Determined Lateral Derivatives of a Swept-Wing Fighter-Type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48. Technical Report NACA RM H56C20, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Asher, William P. (1957) Transonic Flight Evaluation of the Effects of Fuselage Extension and Indentation on the Drag of a 60 Degree Delta-Wing Interceptor Airplane. Technical Report NACA RM H57E29, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Jordan, Gareth H. (1955) Wing Pressure Distributions Over the Lift Range of the Convair XF-92A Delta-Wing Airplane at Subsonic and Transonic Speeds. Technical Report NACA RM H55G07, Research Engineering, NASA Dryden Flight Research Center.
Banner, Richard D. and Reed, Robert D. and Marcy, William L. (1955) Wing-Load Measurements of the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees. Technical Report NACA RM H55A11, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:16:48 PST 2009.
