An analysis of alternatives to provide a varying mach number test capability at APTU

A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 2, Issue , 2006, Pages 1358-1366

  Garrard, Doug ^a,b,c   Seely, Jon ^a,d   Abel, Larry ^a,c,d  

^a ARNOLD ENGINEERING DEVELOPMENT CENTER   (United States)

^b Integrated T and E Department   (United States)

^c AIAA   (United States)

^d MS1400

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT PROPULSION; DECISION THEORY; FLIGHT DYNAMICS; JETS; NOZZLES; TEST FACILITIES;

AERODYNAMIC AND PROPULSION TEST UNIT (APTU); FREEJET NOZZLES; HYPERSONIC AIR BREATHING PROPULSION SYSTEMS; HYPERSONIC PROPULSION TEST CAPABILITY PROJECT;

MACH NUMBER;

EID: 33947207417     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-8044     Document Type: Conference Paper

References (0)