Aerothermodynamics for reusable launch systeme

Aerospace Science and Technology

Volumn 8, Issue 2, 2004, Pages 101-110

  Weiland, C ^a   Longo, J ^b   Gulhan A ^b   Decker, K ^c  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c TECHNICAL UNIVERSITY OF MUNICH   (Germany)

Author keywords

Aerothermodynamics; High enthalpy windtunnel experiments; Hypersonic flow; Numerical simulations; Reusable launch vehicles

Indexed keywords

AERODYNAMICS; AEROSPACE VEHICLES; COMPUTER SIMULATION; ERROR ANALYSIS; HARMONIC ANALYSIS; HYPERSONIC FLOW; THERMODYNAMICS; TRAJECTORIES; WIND TUNNELS;

AEROTHERMODYNAMICS; HIGH ENTHALPY WINDTUNNEL EXPERIMENTS; REUSABLE LAUNCH VEHICLES;

CATAPULTS (AIRCRAFT LAUNCHERS);

EID: 1242310452     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2003.09.003     Document Type: Article

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