Influence of aerodynamic research on the performance of supersonic airplanes von WIMPRESS, JOHN K, SWIHART, JOHN M

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Cost effective, high-technology civil transports von Swihart, John M.

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Method for applying fluid to wire von INAYAT BABER, SWIHART JOHN M, LEACH MATTHEW, CAUDILL GREG S, DETAR MARVIN B

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The United States SST and Air Quality von Swihart, John M.

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Variable Geometry in a Supersonic Transport Aircraft von Swihart, John M.

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Effect of afterbody ejection configurations on the performance at transonic speeds of a pylon-supported Nacelle model having a hot-jet exhaust / by John M. Swihart, Charles E. Merc... von Swihart, John M

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EFFECT OF TARGET-TYPE THRUST REVERSER ON TRANSONIC AERODYNAMIC CHARACTERISTICS OF A SINGLE-ENGINE FIGHTER MODEL von SWIHART, JOHN M

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Investigation at transonic speeds of a fixed divergent ejector installed in a single-engine fighter model / By John M. Swihart and Charles E. Mercer von Swihart, John M

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Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds / John M. Swihart and Norman L. Crabill von Swihart, John M

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Experimental and Calculated Static Characteristics of a Two-blade NACA 10-(3)(062)-045 Propeller von Swihart, John M

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Pressure distributions on three bodies of revolution to determine the effect of Reynolds number up to and including the transonic speed range / by John M. Swihart and Charles F. Wh... von Swihart, John M

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The effect of blade-section camber on the static characteristics of three NACA propellers von Wood, John H, Swihart, John M

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A Hydrogen Peroxide Hot-Jet Simulator for Wind-Tunnel Tests of Turbojet-Exit Models von Runckel, Jack F., Swihart, John M.

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A Hydrogen Peroxide Hot-Jet Simulator for Wind-Tunnel Tests of Turbojet-Exit Models von Runckel, Jack F., Swihart, John M.

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Performance of Multiple Jet-exit Installations von Swihart, John M, Nelson, William J

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Effect of a Hot-jet Exhaust on Pressure Distributions and External Drag of Several Afterbodies on a Single-engine Airplane Model at Transonic Speeds von Norton, Harry T, Jr, Swihart, John M

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Investigation at transonic speeds of a fixed divergent ejector installed in a single-engine fighter model von Swihart, John M, Mercer, Charles E

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Tabulated Pressure Data for a 60 Degree Delta-wing--body--tail Model with a Hot Jet Exhausting from a Pylon-mounted Nacelle von Lee, Edwin E, Jr, Swihart, John M

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A Hydrogen Peroxide Turbojet-engine Simulator for Wind-tunnel Powered-model Investigations von Runckel, Jack F, Swihart, John M

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Transonic Loads Characteristics of a 3-percent-thick 60 Degree Delta-wing--body Combination von Swihart, John M, Foss, Willard E, Jr

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