Wing planform design optimization for reusable launch vehicle

Journal of Aircraft

Volumn 46, Issue 2, 2009, Pages 726-730

  Manokaran, K ^a   Vidya, G ^a   Sivaramakrishnan, A E ^a   Goyal, V K ^a  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CURVE FITTING; HYPERSONIC VEHICLES; OPTIMIZATION; REUSABILITY; SUPERSONIC AIRCRAFT; SURFACE PROPERTIES;

BASELINE CONFIGURATIONS; NUMERICAL OPTIMIZATION TECHNIQUES; OPTIMIZATION TECHNIQUES; PERFORMANCE CONSTRAINTS; RESPONSE SURFACE METHODOLOGY; REUSABLE LAUNCH VEHICLES; STRAIGHT-LINE SEGMENTS; WING PLANFORM DESIGNS;

PLANFORMS;

EID: 63349095021     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.39732     Document Type: Article

References (8)

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3. Manokaran, K., Vidya, C., Sivaramakrishnan, A. E., and Goyal, V. K., "Wing Planform Design Studies for Winged Reusable Launch Vehicle Using Engineering Codes," Proceeding of SAROD-2005, Tata-McGraw Hill, New Delhi, Dec. 2005.
4. Hoak, D. E., "USAF Stability and Control DATCOM," McDonnell Douglas Corporation, NTIS N76-73204, Oct. 1960.
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6. Manokaran, K., Vidya, G., and Goyal, V. K., "A Simple Procedure for Computation of Aerodynamic Coefficients with Control Surface Deflection for a Winged RLV," Proceeding of SAROD-2005, Tata-McGraw Hill, New Delhi, Dec. 2005.
7. Alan, W. W., "Optimum Wing Sizing of a Single-Stage-To-Orbit Vehicle," Journal of Spacecraft and Rockets, Vol. 20, No. 2, March-April 1983, pp. 115-121. doi:10.2514/3.28366
8. Design Expert Ver. 7.1.4, Stat-Ease, Inc., Minneapolis, MN 55413MN 55413.