Incorporation of aerothermodynamic analysis tools into the multi-disciplinary conceptual design process

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 7, Issue , 2007, Pages 4880-4895

  Cunnington, R ^a,b,c,d   Takahashi, T T ^a,b,c,d   Bays, L V ^a,b,c,d  

^a RAYTHEON COMPANY   (United States)

^b MDA/MDO

^c Air Vehicle Product Center

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMODYNAMIC ANALYSIS TOOLS; AEROTHERMODYNAMIC MODELS; THERMAL PROTECTION SYSTEMS;

AIRCRAFT MODELS; MACH NUMBER; MACHINE DESIGN; OPTIMIZATION; TRAJECTORIES; WINGS;

FLIGHT DYNAMICS;

EID: 34347240005     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Office of Manned Vehicles, "Flight Test Results from the Entry and Landing of the Space Shuttle Orbiter for the First Twelve Orbital Flights," Final Report June 1985, AFFTC TR-85-11)
2. Margraves, C. R., S. W. Paris, "Direct trajectory optimization using nonlinear programming and collocation', AIAA J. Guidance, Vol 10, No. 4, p. 338-342, 1987.
3. Fay, J.A. and Riddell, F.R., "Theory of Stagnation Point Heat Transfer in Dissociated Air," J. of the Aeronautical Sciences, Vol. 25, No. 2, Feb. 1958.
4. Hender, D.R., et.al, "A Miniature Version of the JA70 Aerodynamic Heating Computer Program H800 (MINIVER)," MDC Contractor Report G0462, June 1970 (revised)
5. User's Manual for the Aeroheating and Thermal Analysis Code, ATAC03, May 2003, ITTAerotherm, Huntsville, AL.
6. Al Murray, ITT Aerotherm, Huntsville, AL, personal communication.
7. http://www.phoenix-integration.com/modelcenter.htm