Prediction of Drag Reduction in Supersonic and Hypersonic Flows with Counterflow Jets

Prediction of Drag Reduction in Supersonicand Hypersonic Flows with Counterflow JetsEndwell O. DasoBoeing Phantom WorksLong Beach, CaliforniaWarren BeaulieuBoeing Phantom WorksLong Beach, CaliforniaJames O. HagerBoeing Phantom WorksLong Beach, CaliforniaAIAA/AAAF 11th International Space Planesand Hypersonic Systems and TechnologiesConference29 September- 04 October, 2002/Orleans, France

[1]  R. Saeks,et al.  One-dimensional shock characteristics in weakly ionized gases , 1999 .

[2]  G. I. Mishin,et al.  EXPERIMENTAL INVESTIGATION OF THE FLIGHT OF A SPHERE IN WEAKLY IONIZED AIR , 1997 .

[3]  L. Martinelli,et al.  I t SHOCK WAVE PROPAGATION AND STRUCTURE i IN NON-UNIFORM GASES AND PLASMAS , 1999 .

[4]  David J. Romeo,et al.  Flow field for sonic jet exhausting counter to a hypersonic mainstream , 1965 .

[5]  D. Wie,et al.  Shock wave characteristics measured in gas discharges , 1999 .

[6]  E. A. Barber.  An experimental investigation of stagnation- point injection , 1965 .

[7]  David W. Riggins,et al.  Blunt-Body Wave Drag Reduction Using Focused Energy Deposition , 1999 .

[8]  Peter Sherrouse,et al.  Shock Structure of a Spherical Projectile in Weakly Ionized Air , 1999 .

[9]  W. Sears,et al.  The Prospects for Magneto-Aerodynamics , 1958 .

[10]  P. Bletzinger,et al.  Shock wave damping and dispersion in nonequilibrium low pressure argon plasmas , 1997 .

[11]  Z. Bleviss.  Magnetogasdynamics of Hypersonic Couette Flow , 1958 .

[12]  Frank Marconi,et al.  An investigation of tailored upstream heating for sonic boom and drag reduction , 1998 .

[13]  Graham V. Candler,et al.  Effect of internal energy excitation on supersonic air flow , 1999 .

[14]  L. Martinelli,et al.  External control of plasmas for high-speed aerodynamics , 1999 .

[15]  P. J. Finley,et al.  The flow of a jet from a body opposing a supersonic free stream , 1966, Journal of Fluid Mechanics.

[16]  S. Leonov,et al.  INFLUENCE OF A CORONA DISCHARGE ON THE SUPERSONIC DRAG OF AN AXISYJWMETRIC BODY , 1999 .

[17]  J. Shang.  Validation of Plasma Injection for Hypersonic Blunt-Body Drag Reduction , 2003 .

[18]  J. Poggie.  Modeling the effects of weak ionization on supersonic flow and shock waves , 1999 .

[19]  D. Keefer,et al.  Ballistic range tests in weakly ionized argon , 1999 .

[20]  V. I. Lagutin,et al.  Theoretical and experimental study of the possibility of reducing aerodynamic drag by employing plasma injection , 1999 .