Development of the HyShot stability demonstrator

Collection of Technical Papers - 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference

Volumn 1, Issue , 2006, Pages 244-260

  Neuenhahn, Thomas ^a,c,d   Olivier, Herbert ^a,c,d   Paull, Allan ^b,d  

^a RWTH AACHEN UNIVERSITY   (Germany)

^b UNIVERSITY OF QUEENSLAND   (Australia)

^c UNIVERSITY HOSPITAL RWTH AACHEN   (Germany)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC FORCES; FLIGHT STABILITY; FLIGHT TESTS;

FLIGHT DYNAMICS; PARACHUTES; ROCKET ENGINES;

JET AIRCRAFT;

EID: 33751434083     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. th International Space Planes and Hypersonics Systems and Technologies Conference, Capua, Italy, May 16-20,2005, AIAA-2005-3354
2. Settles, G.S. et al.: "Detailed Study of Attached and Separated Compression Corner Flow fields in High Reynolds Number Supersonic Flow," AIAA Journal, Vol. 17, No. 6, June 1979, pp. 579-585
3. Neuenhahn, Thomas: "Lagewinkelbestimmung unter Verwendung eines Magnetometers," Project Work, Chair of Flight Dynamics, RWTH Aachen University, Germany, 2004