Hypersonic drag and heat-transfer reduction using a forward-facing jet

Journal of Aircraft

Volumn 38, Issue 4, 2001, Pages 680-686

  Meyer, Benjamin ^a   Nelson, H F ^a   Riggins, David W ^a  

^a MISSOURI UNIVERSITY OF SCIENCE AND TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; FRICTION; HEAT TRANSFER; JETS; NAVIER STOKES EQUATIONS; STABILITY; THERMAL CONDUCTIVITY; TWO DIMENSIONAL; VISCOSITY;

BLUNT BODY; FORWARD FACING JET; HEAT TRANSFER REDUCTION; HYPERSONIC DRAG; SKIN FRICTION DRAG; STAGNATION POINT;

AIRCRAFT;

EID: 0035390014     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2819     Document Type: Article

References (13)

1. Forward facing spike effects of bodies of different cross section in supersonic flow
2. Numerical investigation of supersonic flows around a spiked blunt body
3. Blunt body wave drag reduction using focused energy deposition
4. Experimental pressure investigation of a ’Directed-energy air spike’ inlet at Mach 10
5. Experimental heat transfer investigation of a ’Directed-energy air spike’ inlet at Mach 10
6. Flow features of shock-induced combustion around projectile traveling at hypervelocities
7. A detailed numerical model of a supersonic mixing layer
8. The flow of a jet from a body opposing a supersonic free stream
9. Shock wave shapes around spherical- and cylindrical-nosed bodies