Detailed aerodynamic design optimization of an RLV turbine

37th Joint Propulsion Conference and Exhibit

Volumn , Issue , 2001, Pages

  Griffin, Lisa W ^a   Dorney, Daniel J ^a   Huber, Frank W ^b   Tran, Ken ^c   Shyy, Wei ^d   Papila, Nilay ^d  

^a NASA MARSHALL SPACE FLIGHT CENTER   (United States)

^b Riverbend Design Services Inc   (United States)

^c BOEING COMPANY   (United States)

^d University of Florida   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADVANCED ANALYTICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE REUSABILITY; DESIGN; EFFICIENCY; NASA; PROPULSION; REUSABILITY; SPACE FLIGHT; SUPERSONIC AIRCRAFT; TURBINES;

ADVANCED DESIGNS; AERODYNAMIC DESIGN OPTIMIZATION; ITS APPLICATIONS; OPTIMIZED DESIGNS; OPTIMUM DETAILED DESIGN; RE-USABLE LAUNCH VEHICLES (RLV); SUPERSONIC DESIGNS; TURBINE AERODYNAMICS;

AERODYNAMICS;

EID: 85085778520     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-3397     Document Type: Conference Paper

References (16)

1. Huber, Frank, "Turbine Aerodynamic Design Tool Development", presented at the Space Transportation Fluids Workshop, Marshall Space Flight Center, AL, April 2001
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3. Vaidyanathan, Rajkuma, Papila, Nilay, Shyy, Wei, Tucker, Kevin, Griffin, Lisa, Haftka, Raphael, and Fitz-Coy, Norman, "Neural Network and Response Surface Methodology for Rocket Engine Component Optimization", AIAA Paper 2000- 4880, September 2000.
4. th Annual Symposium on Propulsion, Cleveland, OH, October 2000.
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12. Dorney, D. J., and Davis, R. L, "Numerical Simulation of Turbine "Hot Spot" Alleviation Using Film Cooling," AIAA Journal of Propulsion and Power. Vol 9, No.3, May-June 1993, pp. 329-336.
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16. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January, 2002.