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ICAS Secretariat - 26th Congress of International Council of the Aeronautical Sciences 2008, ICAS 2008

Volumn 6, Issue , 2008, Pages 272-305

Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods

(2) Erickson, Gary E a DeLoach, Richard a

a NASA LANGLEY RESEARCH CENTER (United States)

Author keywords

Multi stage launch vehicles; Response surface methods; Shock waves; Stage separation aerodynamics; Supersonic speeds; Wind tunnel testing

Indexed keywords

MULTI-STAGE; RESPONSE SURFACE METHOD; STAGE SEPARATION; SUPERSONIC SPEED; WIND-TUNNEL TESTING;

COPYRIGHTS; DESIGN; LAUNCH VEHICLES; PAPER; SEPARATION; SHOCK WAVES; SURFACE PROPERTIES;

AERODYNAMIC CONFIGURATIONS;

EID: 84878465027 PISSN: None EISSN: None Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper

Times cited : (8)

References (20)

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