Dryden Technical Report Server
From the NTRS FAQ: Where do I go for a hardcopy of the report?
- STABILITY AND CONTROL MEASUREMENTS OBTAINED DURING USAF-NACA COOPERATIVE FLIGHT-TEST PROGRAM ON THE X-4 AIRPLANE (USAF NO. 46-677) , Research Memorandum
Authors: Melvin Sadoff, Herman O. Ankenbruck and William O’Hare
Report Number: NACA-RM-A51H09
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: October 1951
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II (BUAERO NO. 37974) RESEARCH AIRPLANE: STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS AT MACH NUMBERS UP TO 0.87 , Research Memorandum
Authors: S. A. Sjoberg, James R. Peele and John H. Griffith
Report Number: NACA-RM-L50K13
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: January 1951
- FLIGHT DETERMINATION OF THE EFFECTS OF WING VORTEX GENERATORS ON THE AERODYNAMIC CHARACTERISTICS OF THE DOUGLAS D-558-I AIRPLANE , Research Memorandum
Authors: De E. Beeler, Donald R. Bellman and John H. Griffith
Report Number: NACA-RM-L51A23
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: August 1951
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-1 AIRPLANE IN AN UNACCELERATED STALL AND IN PULL-UPS AT MACH NUMBERS OF 0.74, 0.75, 0.94, AND 0.97 , Research Memorandum
Authors: Lawrence A. Smith
Report Number: NACA-RM-L51B23
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: June 1951
- FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-II (BUAERO NO. 37974) RESEARCH AIRPLANE: DYNAMIC LATERAL STABILITY , Research Memorandum
Authors: W. H. Stillwell and J. V. Wilmerding
Report Number: NACA-RM-L51C23
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: June 1951
- FLIGHT INVESTIGATION OF THE LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF THE DOUGLAS D-558-I AIRPLANE (BUAERO NO. 37972) AT MACH NUMBERS UP TO 0.89 , Research Memorandum
Authors: Mrlvin Sadoff, William S. Roden and John M. Eggleston
Report Number: NACA-RM-L51D18
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: June 1951
- LIFT AND DRAG COEFFICIENTS FOR THE BELL X-1 AIRPLANE (8-PERCENT-THICK WING) IN POWER-OFF TRANSONIC FLIGHT
Authors: L. Robert Carman and John R. Carden
Report Number: NACA-RM-L51E08
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: June 1951
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED IN FLIGHT ON THE WING OF THE D-558-I RESEARCH AIRPLANE THROUGH A MACH NUMBER RANGE OF 0.80 TO 0.89 AND THROUGHOUT THE NORMAL-FORCE-COEFFICIENT RANGE AT MACH NUMBERS OF 0.61, 0.70, 0. , Research Memorandum
Authors: Earl R. Keener and Rozalia M. Bandish
Report Number: NACA-RM-L51F12
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: August 1951
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-1 AIRPLANE IN AN UNACCELERATED LOW-SPEED STALL, IN PUSH-OVERS AT MACH NUMBERS OF 0.83 AND 0.99, AND IN A PULL-UP AT A MACH NUMBER OF 1.16 , Research Memorandum
Authors: Ronald J. Knapp
Report Number: NACA-RM-L51F24
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: September 1951
- TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-1 AIRPLANE IN AN UNACCELERATED LOW-SPEED STALL, IN PUSH-OVERS AT MACH NUMBERS OF 0.83 AND 0.99, AND IN A PULL-UP AT A MACH NUMBER OF 1.16 , Research Memorandum
Authors: Ronald J. Knapp
Report Number: NACA-RM-L51F25
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: September 1951
- ANALYSIS OF LONGITUDINAL STABILITY AND TRIM OF THE BELL X-1 AIRPLANE AT A LIFT COEFFICIENT OF 0.3 TO MACH NUMBERS NEAR 1.05 , Research Memorandum
Authors: Hubert M. Drake, John R. Carden and Harry P. Clagett
Report Number: NACA-RM-L51H01
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: October 1951
|