Wind-tunnel results of the B-52B with the X-43A stack

Journal of Spacecraft and Rockets

Volumn 44, Issue 4, 2007, Pages 871-877

  Davis, Mark C ^a,d,e   Sim, Alexander G ^a,d,e   Rhode, Matthew ^b,d,e   Johnson Sr , Kevin D ^c,e,f  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c NASA HEADQUARTERS   (United States)

^d Medium Speed Wind Tunnel

^e AIAA   (United States)

^f Research Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; LAUNCHING; ROCKETS; STREAM FLOW; STRUCTURAL LOADS;

AERODYNAMIC INFLUENCE; LAUNCH VEHICLES; ROLLING MOMENTS;

WIND TUNNELS;

EID: 34548345819     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.27191     Document Type: Article

References (3)

1. Adolph, C. E., Allavie, J. E., and Bock, C. C., Jr., "Flight Evaluation of the B-52 Carrier Aircraft for the X-15," U.S. Air Force Flight Test Center Rept. TR-60-33, Edwards AFB, CA, Sept. 1960.
2. Freeman, D., Reubush, D., McClinton, C., Rausch, V., and Crawford, L., "The Hyper-X Program," NASA TM-97-207243, 1997.
3. Dominguez, K., Graham, A. B., and DeLoach, R., "Development of an MDOE Compliant Control System in the ViGYAN Low-Speed Wind Tunnel," AIAA Paper 2001-0169, 2001.