Stabilization of hypersonic boundary layers by porous coatings

AIAA Journal

Volumn 39, Issue 4, 2001, Pages 605-610

  Fedorov, Alexander V ^a   Malmuth, Norman D ^b   Rasheed, Adam ^c   Hornung, Hans G ^c  

^a MOSCOW INSTITUTE OF PHYSICS AND TECHNOLOGY   (Russian Federation)

^b ROCKWELL SCIENCE CENTER   (United States)

^c CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CYLINDERS (SHAPES); ENERGY ABSORPTION; ENTHALPY; HYPERSONIC AERODYNAMICS; LAMINAR FLOW; MICROPOROUS MATERIALS; REYNOLDS NUMBER; STABILITY;

THERMAL PROTECTION SYSTEM (TPS);

BOUNDARY LAYERS;

EID: 0035311397     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1382     Document Type: Article

References (24)

1. Boundary-layer stability theory
2. Stability theory as a guide to the evaluation of transition data
3. Prediction and control of transition in supersonic and hypersonic boundary layers
4. Stability theory for laminar flow control design
5. Wind-tunnel experiments relating to supersonic and hypersonic boundary-layer transition
6. Influence of porous layer on boundary-layer stability
7. Influence of gas compressibility on stability of boundary layer on porous surface at subsonic speeds
8. Stability of supersonic boundary layer on porous wall with heat conductivity
9. Propagation of sound and the assignment of shape factors in model porous materials having simple pore geometries
10. On the propagation of sound waves in a cylindrical conduit
11. On the propagation of sound waves in a cylindrical conduit
12. Stability of the inviscid shock layer in strong interaction flow over a hypersonic flat plate