Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga.

Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer.

Ferguson, Harold.
Schaefer, John W.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Atmosp...

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski.

Becker, John V.
Korycinski, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Intrieri, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Exploratory tests of the effects of jet plumes on the flow over cone-cylinder-flare bodies /

Falanga, Ralph A.
Crawford, Davis H.
Hinson, William F.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles.Includes bibliographical refer...

Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds /

Ladson, Charles L.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Simulators an...

Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ /

Penland, Jim A.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles;Includes bibliographical reference...

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer.

Ferguson, Harold.
Schaefer, John W.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Atmosp...

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski.

Becker, John V.
Korycinski, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Intrieri, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Exploratory tests of the effects of jet plumes on the flow over cone-cylinder-flare bodies /

Falanga, Ralph A.
Crawford, Davis H.
Hinson, William F.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles.Includes bibliographical refer...

Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds /

Ladson, Charles L.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Simulators an...

Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ /

Penland, Jim A.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles;Includes bibliographical reference...

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer.

Ferguson, Harold.
Schaefer, John W.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Atmosp...

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski.

Becker, John V.
Korycinski, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga.

Abstract

Extracted data

Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga.

Abstract

Extracted data

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