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- STALL CHARACTERISTICS OBTAINED FROM FLIGHT 10 OF NORTHROP X-4 NO. 2 AIRPLANE (USAF NO. 46-677)
Authors: Melvin Sadoff and Thomas R. Sisk
Report Number: NACA-RM-A50A04
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1950
No. Pages: 23
- LONGITUDINAL-STABILITY CHARACTERISTICS OF THE NORTHROP X-4 AIRPLANE (USAF NO. 46-677)
Authors: Melvin Sadoff and Thomas R. Sisk
Report Number: NACA-RM-A50D27
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: June 1950
No. Pages: 23
- SUMMARY REPORT OF RESULTS OBTAINED DURING DEMONSTRATION TESTS OF THE NORTHROP X-4 AIRPLANES
Authors: Melvin Sadoff and Thomas R. Sisk
Report Number: NACA-RM-A50I01
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: December 1950
No. Pages: 45
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II (BUAERO NO. 37974) RESEARCH AIRPLANE STATIC LATERAL AND DIRECTRIONAL STABILITY CHARACTERISTICS AS MEASURED IN SIDESLIPS AT MACH NUMBERS UP TO 0.87
Authors: S. A. Sjoberg
Report Number: NACA-RM-L50C14
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1950
No. Pages: 28
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II (BUAERO NO. 37974) RESEARCH AIRPLANE. DETERMINATION OF THE AERODYNAMIC CENTER AND ZERO-LIFT PITCHING-MOMENT COEFFICIENT OF THE WING-FUSELAGE COMBINATION BY MEANS OF TAIL-LOAD MEASUREMENTS IN THE MACH NUMBER RA , Research Memorandum
Authors: John P. Mayer, George M. Valentine and Geraldine C. Mayer
Report Number: NACA-RM-L50D10
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 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
Authors: Jim Rogers Thompson, William S. Roden and John M. Eggleston
Report Number: NACA-RM-L50D20
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1950
No. Pages: 21
- 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
Authors: J.V. Wilmerding, W.H. Stillwell and S.A. Sjoberg
Report Number: NACA-RM-L50E17
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1950
No. Pages: 25
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II BUAERO NO. 37974 RESEARCH AIRPLANE. MEASUREMENTS OF THE BUFFET BOUNDARY AND PEAK AIRPLANE NORMAL FORCE COEFFICIENTS AT MACH NUMBERS UP TO 0.90 , Research Memorandum
Authors: John P. Mayer and George M. Valentine
Report Number: NACA-RM-L50E31
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: August 1950
- EFFECT OF AN AUTOPILOT SENSITIVE TO YAWING VELOCITY ON THE LATERAL STABILITY OF THE DOUGLAS D-558-II AIRPLANE , Research Memorandum
Authors: Ordway B. Gates and Leonard Sternfield
Report Number: NACA-RM-L50F22
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: August 1950
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II (BUAERO NO. 37974) RESEARCH AIRPLANE LOW-SPEED STALLING AND LIFT CHARACTERISTICS
Authors: W. H. Stillwell, J. V. Wilmerding and R. A. Champine
Report Number: NACA-RM-L50G10
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1950
No. Pages: 38
- ELEVATOR-STABILIZER EFFECTIVENESS AND TRIM OF THE X-1 AIRPLANE TO A MACH NUMBER OF 1.06
Authors: Hubert M. Drake and John R. Carden
Report Number: NACA-RM-L50G20
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1950
No. Pages: 13
- 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
Authors: H. Arthur Carner and Ronald J. Knapp
Report Number: NACA-RM-L50H04
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1950
No. Pages: 25
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II (BUAERO NO. 37974) RESEARCH AIRPLANE: MEASUREMENTS OF WING LOADS AT MACH NUMBERS UP TO 0.87 , Research Memorandum
Authors: John P. Mayer, George M. Valentine and Beverly J. Swanson
Report Number: NACA-RM-L50H16
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: December 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
Authors: H. Arthur Carner and Mary M. Payne
Report Number: NACA-RM-L50H25
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1950
No. Pages: 43
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-1 AIRPLANE IN PULL-UPS AT MACH NUMBERS FROM 0.53 TO 0.99 , Research Memorandum
Authors: Ronald J. Knapp and Gertrude V. Wilken
Report Number: NACA-RM-L50H28
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1950
- EFFECTS ON THE LATERAL OSCILLATION OF FIXING THE RUDDER AND REFLEXING THE FLAPS ON THE BELL X-1 AIRPLANE
Authors: Hubert M. Drake
Report Number: NACA-RM-L50I05
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: December 1950
No. Pages: 13
- 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
Authors: Ellwyn E. Angle and Euclid C. Holleman
Report Number: NACA-RM-L50I06A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1950
No. Pages: 23
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED IN FLIGHT ON THE WING OF THE DOUGLAS D-558-I AIRPLANE FOR A 1 G STALL, A SPEED RUN TO A MACH NUMBER OF 0.90, AND A WIND-UP
Authors: Earl R. Keener and Mary Pierce
Report Number: NACA-RM-L50J10
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: December 1950
No. Pages: 40
- 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 UPS UP TO 0.87
Authors: John P. Mayer and George M. Valentine
Report Number: NACA-RM-L50J13
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1950
No. Pages: 31
- EFFECTS ON THE SNAKING OSCILLATION OF THE BELL X-1 AIRPLANE OF A TRAILING-EDGE BULB ON THE RUDDER
Authors: Hubert M. Drake and Harry P. Clagett
Report Number: NACA-RM-L50K01A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1950
No. Pages: 13
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED IN FLIGHT ON THE WING OF 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
Authors: Earl R. Keener, James R. Peele and Julia B. Woodbridge
Report Number: NACA-RM-L50L12A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1950
No. Pages: 37
- RESULTS OBTAINE DURING FLIGHTS 1 TO 6 OF THE NORTHROP X-4 AIRPLANE (A.F. NO. 46-677)
Authors: James T. Matthews, Jr.
Report Number: NACA-RM-L9K22
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1950
No. Pages: 17
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