Equations for the Newtonian static and dynamic aerodynamic coefficients for a body of revolution with an offset center-of-gravity location /

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...

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...

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

Working charts for rapid prediction of force and pressure coefficients on arbitrary bodies of revolution by use of Newtonian concepts /

Rainey, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Bodies, aerodynamic theory; Aerodynamic loads, bodies.Includes bibliogra...

Forces and moments on sphere-cone bodies in Newtonian flow /

Dickey, Robert R.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mech...

Aerodynamic-center considerations of wings and wing-body combinations /

Lamar, John E.
Alford, William J.
United States. National Aeronautics and Space Administration.

Cover title."October 1966."Includes bibliographical references.Mode of access: Internet

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data /

Wells, William R.
Armstrong, William O.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1962

Cover title.Includes bibliographical references (p. 42-43).Mode of access: Internet

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

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...

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...

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...

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

Working charts for rapid prediction of force and pressure coefficients on arbitrary bodies of revolution by use of Newtonian concepts /

Rainey, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Bodies, aerodynamic theory; Aerodynamic loads, bodies.Includes bibliogra...

Forces and moments on sphere-cone bodies in Newtonian flow /

Dickey, Robert R.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mech...

Aerodynamic-center considerations of wings and wing-body combinations /

Lamar, John E.
Alford, William J.
United States. National Aeronautics and Space Administration.

Cover title."October 1966."Includes bibliographical references.Mode of access: Internet

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data /

Wells, William R.
Armstrong, William O.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1962

Cover title.Includes bibliographical references (p. 42-43).Mode of access: Internet

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

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...

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...

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...

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

Equations for the Newtonian static and dynamic aerodynamic coefficients for a body of revolution with an offset center-of-gravity location /

Abstract

Extracted data

Equations for the Newtonian static and dynamic aerodynamic coefficients for a body of revolution with an offset center-of-gravity location /

Abstract

Extracted data

Related items

Related items