Influence of laminar boundary-layer transition on entry vehicle designs

Journal of Spacecraft and Rockets

Volumn 45, Issue 2, 2008, Pages 165-175

  Lin, T C ^a,b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b Mission System Missile Engineer Center

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; LAMINAR FLOW; PARAMETER ESTIMATION; TURBULENT FLOW;

AERODYNAMIC STABILITY DEGRADATION; ENTRY VEHICLE DESIGNS; HEATING AUGMENTATION; LAMINAR BOUNDARY-LAYER TRANSITION;

TRANSITION FLOW;

EID: 42949144106     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.30047     Document Type: Conference Paper

References (30)