Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Approximate analysis of G loads and heating during atmospheric entries and passes with constant aerodynamic coefficients Roger W. Luidens.

Luidens, Roger W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Atmospheric entry; Space mechanics.Includes bibliographical references.Mode ...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mecha...

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

Levy, Lionel L.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Experimental and theoretical study of heat conduction for air up to 5000 degrees F /

Peng, Tzy-Cheng.
Ahtye, Warren F.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Chemical engineering; Chemist...

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

Regime of frozen boundary layers in stagnation region of blunt reentry bodies /

Grier, Norman T.
Sands, Norman.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry' Fluid mechanics...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Approximate analysis of G loads and heating during atmospheric entries and passes with constant aerodynamic coefficients Roger W. Luidens.

Luidens, Roger W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Atmospheric entry; Space mechanics.Includes bibliographical references.Mode ...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mecha...

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

Levy, Lionel L.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Experimental and theoretical study of heat conduction for air up to 5000 degrees F /

Peng, Tzy-Cheng.
Ahtye, Warren F.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Chemical engineering; Chemist...

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

Regime of frozen boundary layers in stagnation region of blunt reentry bodies /

Grier, Norman T.
Sands, Norman.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry' Fluid mechanics...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Abstract

Extracted data

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Abstract

Extracted data

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