Comptes Rendus
Comparison between methods of generation of waveriders derived from conical flows
[Comparaison de méthodes de génération de waveriders derivés d'écoulements coniques]
Comptes Rendus. Mécanique, Volume 334 (2006) no. 2, pp. 117-122.

Les waveriders sont des configurations portantes supersoniques ou hypersoniques qui sont générées à partir d'un écoulement connu empêchant tout déversement latéral de la zone haute pression de l'intrados vers l'extrados assurant ainsi de hautes finesses. Une méthode utilisant un code Euler est utilisée pour étudier des waveriders créés à partir d'écoulements axisymétriques. Dans le cas du cône, les résultats sont comparés avec ceux du système de Taylor–Maccoll et de la théorie des petites perturbations hypersoniques. Dans les conditions de la présente étude à Mach 5 la dernière méthode fournit paradoxalement des résultats comparables à ceux de Taylor–Maccoll aux grands angles de cône (supérieurs à 10°) tandis que la meilleure finesse est obtenue pour de petits angles.

Waveriders are supersonic or hypersonic lifting configurations which are generated from a known flowfield, preventing leakage from the high-pressure undersurface to the uppersurface, and allowing high lift-to-drag ratios. A method based on an Euler code is used to study waveriders generated from the flow field around axisymmetric bodies. In the case of a cone, the results are compared with those given by the Taylor–Maccoll system and inviscid hypersonic small-disturbance theory. In the present study conditions at Mach 5, the last method paradoxically works at high cone angles (greater than 10°) while the best lift-to-drag ratio are obtained with small angles.

Reçu le :
Accepté le :
Publié le :
DOI : 10.1016/j.crme.2006.01.003
Keywords: Fluid mechanics, Hypersonic, Waveriders, Cone, Small-disturbances, Lift-to-drag ratio
Mots-clés : Mécanique des fluides, Hypersonique, Waveriders, Cône, Petites perturbations, Finesse

Bruno Mangin 1 ; Amer Chpoun 1 ; Richard Benay 2 ; Bruno Chanetz 2

1 Laboratoire d'aérothermique, CNRS, 1C, avenue de la recherche scientifique, 45077 Orléans, France
2 ONERA DAFE, 8, rue des Vertugadins, 92190 Meudon, France
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Bruno Mangin; Amer Chpoun; Richard Benay; Bruno Chanetz. Comparison between methods of generation of waveriders derived from conical flows. Comptes Rendus. Mécanique, Volume 334 (2006) no. 2, pp. 117-122. doi : 10.1016/j.crme.2006.01.003. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2006.01.003/

[1] T.R.F. Nonweiler Delta wings of shape amenable to exact shock wave theory, J. Royal Aero. Soc., Volume 67 (1963), p. 39

[2] D. Kuchemann The Aerodynamic Design of Aircraft, Pergamon Press, Oxford, 1978, pp. 448-510

[3] S. Corda, J.D. Anderson, Viscous optimized hypersonic waveriders designed from axisymmetric flowfields, AIAA-88-0369, January 1988

[4] K.G. Bowcutt, J.D. Anderson, D. Capriotti, Viscous optimized hypersonic waveriders, AIAA-87-0272

[5] B. Mangin, R. Benay, B. Chanetz, Augmentation de la finesse d'un engin hypersonique par application du concept “Waveriders”, ONERA-RT 5/08424 DAFE, 2003

[6] M.J. Zucrow, J.D. Hoffman, Gas Dynamics, vols. 1, 2, John Wiley & Sons, New York

[7] M.L. Rasmussen, Analysis of cone-derived waveriders by hypersonic small-disturbance theory, in: Proceedings of the First International Hypersonic Waverider Symposium, October 1990

[8] E.R.G. Eckert Engineering relations for heat transfer and friction in high-velocity laminar and turbulent boundary layer flow over surfaces with constant pressure and temperature, Trans. Amer. Soc. Mech. Engrg., Volume 78 (1956) no. 6, pp. 1273-1283

[9] J. Cousteix Turbulence et couche limite, Cépaduès, 1989

[10] P.C. Stainback, R.D. Wagner, F.K. Owen, C.C. Horstman, Experimental studies of hypersonic boundary-layer transition and effects of wind-tunnel disturbances, NASA TND 7453, 1974

[11] J.D. Anderson Hypersonic and High Temperature Gas Dynamics, McGraw-Hill, 1989

[12] M. Lobbia, K. Suzuki, Design and analysis of payload-optimized waveriders, AIAA 2001-1849, 2001

[13] B. Mangin, R. Benay, B. Chanetz, A. Chpoun, Optimization of viscous Mach 5 waveriders derived from axisymmetric power-law blunt body flows, Journal of Spacecraft and Rockets, September 2005, submitted for publication

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