Numerical simulations of an oblique detonation wave engine von Cambier, Jean-Luc, Adelman, Henry, Menees, Gene P

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Aerothermodynamics of transatmospheric vehicles von Tauber, Michael E, Menees, Gene P, Adelman, Henry G

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Wave combustors for trans-atmospheric vehicles von Menees, Gene P, Adelman, Henry G, Cambier, Jean-Luc, Bowles, Jeffrey V

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Bent-biconic single-stage-to-orbit vehicle conceptual study von Park, Chul, Menees, Gene P, Bowles, Jeffrey V, Lawrence, Scott L, Davies, Carol B

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Numerical simulations of oblique detonations in supersonic combustion chambers von Cambier, Jean-Luc, Adelman, Henry G, Menees, Gene P

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Trajectory analysis of radiative heating for planetary missions withaerobraking of spacecraft von Menees, Gene P

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Nitric oxide formation by meteoroids in the upper atmosphere von Menees, Gene P., Park, Chul

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Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept von Menees, Gene P, Brown, Kevin G, Wilson, John F, Davies, Carol B

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Ascent aeromaneuvering capabilities of transatmospheric vehicles von Menees, Gene P, Tauber, Michael E, Wilson, John T, Adelman, Henry G

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Determining atmospheric density using a space-launched projectile von Menees, Gene P, Park, Chul, Brown, Kevin G, Wilson, John F

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Aeroassisted-vehicle design studies for a manned Mars mission von Menees, Gene P.

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Trajectory analysis of radiative heating for planetary missions with aerobraking of spacecraft von Menees, G. P.

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Lift, Drag, and Pitching Moment of an Aspect-Ratio-2 Triangular Wing with Leading-Edge Flaps Designed to Simulate Conical Camber von Menees, Gene P.

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A method for computing the nonequilibrium radiant emission from near-equilibrium shock layers von MENEES, GENE P.

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Analytical and experimental investigations of the oblique detonation wave engine concept von Menees, Gene P., Adelman, Henry G., Cambier, Jean-Luc

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The Use of Steady and Pulsed Detonations for Propulsion Systems von Adelman, Henry G., Menees, Gene P., Cambier, Jean-Luc, Bowles, Jeffrey V.

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A simplified chemical model for estimating the nonequilibrium radiant emission of CN /violet/ in shock-heated mixtures of CO sub 2 and N sub 2 von MENEES, GENE P., McKENZIE, ROBERT L.

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AERODYNAMIC LOADS AT MACH NUMBERS FROM 0.70 TO 2.22 ON AN AIRPLANE MODEL HAVING A WING AND CANARD OF TRIANGULAR PLAN FORM AND EITHER SINGLE OR TWIN VERTICAL TAILS von PETERSON,VICTOR L, MENEES,GENE P

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Aerodynamic Loads at Mach Numbers from 0.70 to 2.22 on an Airplane Model Having a Wing and Canard of Triangular Plan Form and Either Single or Twin Vertical Tails Supplement I-Tabu... von Peterson, Victor L., Menees, Gene P.

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Aerodynamic Loads at Mach Numbers from 0.70 to 2.22 on a Airplane Model Having a Wing and Canard of Triangular Plan Form and Either Single or Twin Vertical Tails von Peterson, Victor L., Menees, Gene P.

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