Sustained Hypersonic Flight Experiment (SHyFE)

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

Volumn 1, Issue , 2006, Pages 215-226

  Dadd, Graham J ^a,b   Owen, Rachel E ^a,b   Hodges, John ^a,b   Atkinson, Keith N ^a,b  

^a QINETIQ   (United Kingdom)

^b SHyFE ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

DE-RISKING; HIGH TEMPERATURE MATERIALS; QINETIQ (CO);

COMPUTATIONAL FLUID DYNAMICS; FLIGHT DYNAMICS; MACH NUMBER; ROCKET ENGINES; SPACECRAFT PROPULSION;

HYPERSONIC FLOW;

EID: 33947280991     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. th AIAA International Space Planes and Hypersonics Systems and Technologies Conference, AIAA 2003-7030, 2003
2. Veraar, R. G., and Mayer, A. E. H. J., "High Speed Air Breathing Propulsion System Research and Development at TNO," RTO-MP-AVT-135 No.20. 2006.
3. Blake, W. B., "Missile DATCOM User's Manual - 1997 FORTRAN90 Revision," Air Force Laboratory, USA, TANW-TR-97-001 A, 1997.
4. Ludlow, D. K., "IMPNS Theory Guide", DERA/MSS/MSFC2/TR010713, 2001.
5. Boon, S., "Numerical Analysis of Hypersonic Inlet Flows," PhD thesis, Imperial College London, England (to be published).