Hypersonic viscous static stability of a sharp 5-deg cone at incidence
| Autor: | J. C. Adams, B. J. Griffith |
|---|---|
| Rok vydání: | 1976 |
| Předmět: |
Hypersonic speed
Stagnation temperature Mathematical optimization Materials science Angle of attack Longitudinal static stability Aerospace Engineering Reynolds number Laminar flow Mechanics Physics::Fluid Dynamics symbols.namesake Inviscid flow Physics::Space Physics symbols Hypersonic wind tunnel Physics::Chemical Physics |
| Zdroj: | AIAA Journal. 14:1062-1068 |
| ISSN: | 1533-385X 0001-1452 |
| DOI: | 10.2514/3.7186 |
| Popis: | Static stability characteristics of a 5-deg semivertex angle sharp cone at angles of attack up to 4 deg are examined both theoretically and experimentally under hypersonic wind tunnel conditions. Interpretation of the experimental results is based upon a three-dimensional inviscid/laminar boundary-layer analysis and a threedimensional hypersonic viscous shock layer analysis. It is shown that only the three-dimensional hypersonic viscous shock layer approach is capable of accurately predicting the static stability characteristics of a sharp cone at incidence under low Reynolds number hypersonic flow conditions where three-dimensional viscous interaction effects are dominant. Also considered are wall temperature effects on sharp cone at incidence static stability relative to extrapolation of hot-wall hypersonic wind tunnel results to cold-wall flight conditions. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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