Hypersonic effectiveness of slender lifting elliptic cones with and without strakes

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Kontis, K ^a   Stollery, J L ^a   Edwards, J A ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYERS; REYNOLDS NUMBER;

SURFACE FLOW;

LAMINAR BOUNDARY LAYER;

EID: 84983134622     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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2. Wells, W. and Armstrong, W.: Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spherical bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data.NASATRR-127, 1961.
3. Stetson, K. F: Experimental results of laminar boundary layer separation on a slender cone at angle of attack at MM.WPAFB, ARL 71-0127, 1971.
4. Peake, D. J. and Tobak, M.:Three-dimensional flows about simple components at angle of attack.AGARD LS-121,1982.
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6. Kontis, K. and Stollery J. L.:Control effectiveness of a jet-slender body combination at hypersonic speeds.AIAA 96-2470, 1996.
7. Fournier, R. H. and Spencer, B, Jr.: Supersonic aerodynamic characteristics of a series of related bodies of circular and elliptical cross section.NASA TN D-3539, 1966.
8. Fox, C. H. Jr. and Spencer, B. Jr.:Hypersonic aerodynamic characteristics of low-wave-drag elliptical-body-tail combinations as affected by changes in stabiliser configuration.NASA TM X-1620,1968.
9. Sigal, A.rMethods of analysis and experiments for missiles with non-circular fuselages.Tactical Missile Aerodynamics, prediction methodology. Edited by Mendenhall, M. R., 2nd edition, 1992.
10. Reggiori, A.:Lift and drag of wing-cone configuration in hypersonic flow.AIAA Journal, vol. 9, no. 4, 1971.