X-34 vehicle aerodynamic characteristics

Journal of Spacecraft and Rockets

Volumn 36, Issue 2, 1999, Pages 229-239

  Brauckmann, Gregory J ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE VELOCITY; AIRCRAFT PARTS AND EQUIPMENT; DRAG; FLIGHT DYNAMICS; REYNOLDS NUMBER; SPACE FLIGHT; SUPERSONIC AERODYNAMICS; TRAJECTORIES; TRANSONIC AERODYNAMICS; WIND TUNNELS;

AERODYNAMIC PROPERTIES; BODY FLAP DEFLECTION; ELEVON DEFLECTION; LONGITUDINAL CONTROL EFFECTIVENESS; LONGITUDINAL TRIM; MACH NUMBER; REACTION CONTROL JET; RUDDER DEFLECTION;

AEROSPACE VEHICLES;

EID: 0033099115     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3453     Document Type: Article

References (5)

1. Lindberg, R. E., and Feconda, R. T., "X-34: A Test Bed for RLV Technology," Aerospace America, Aug. 1998, pp. 30-33.
2. McGhee, R. J., Beasley, W. D., and Foster, J. M., "Recent Modifications and Calibration of the Langley Low-Turbulence Pressure Tunnel," NASA TP-2328, July 1984.
3. Capone, F. J., Bangert, L. S., Asbury, S. C., Mills, C. T., and Bare, E. A., "The NASA Langley 16-Foot Transonic Tunnel," NASA TP-3521, Sept. 1995.
4. Jackson, C. M., Corlett, W. A., and Monta, W. J., "Description and Calibration of the Langley Unitary Plan Wind Tunnel," NASA TP-1905, Nov. 1981.
5. Micol, J. M., "Hypersonic Aerodynamic/Aero-Thermodynamic Testing Capabilities at Langley Research Center: Aerothermodynamic Facilities Complex," AIAA Paper 95-2107, June 1995.