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

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...

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...

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...

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

Ried, Robert C.
Mayo, Edward E.
United States. National Aeronautics and Space Administration.

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

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...

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...

Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges /

Margolis, Kenneth.
Elliott, Miriam H.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and load...

Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. /

Henderson, Arthur, 1922-
Braswell, Dorothy O.
United States. National Aeronautics and Space Administration.

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

Some simple solutions to the problem of predicting boundary-layer self-induced pressures /

Bertram, Michael H.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

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

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

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...

Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack /

Jorgensen, Leland H.
United States. National Aeronautics and Space Administration.

Issued Sept. 1977.Includes bibliographical references (p. 68-74).Mode of access: Internet

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

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

Development of aerodynamic prediction methods for irregular planform wings /

Benepe, David B.
General Dynamics Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."February 1983"--Cover."General Dynamics."Includes bibliographical references.Mo...

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

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...

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...

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...

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

Ried, Robert C.
Mayo, Edward E.
United States. National Aeronautics and Space Administration.

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

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...

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...

Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges /

Margolis, Kenneth.
Elliott, Miriam H.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and load...

Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. /

Henderson, Arthur, 1922-
Braswell, Dorothy O.
United States. National Aeronautics and Space Administration.

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

Some simple solutions to the problem of predicting boundary-layer self-induced pressures /

Bertram, Michael H.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

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

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

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...

Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack /

Jorgensen, Leland H.
United States. National Aeronautics and Space Administration.

Issued Sept. 1977.Includes bibliographical references (p. 68-74).Mode of access: Internet

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

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

Development of aerodynamic prediction methods for irregular planform wings /

Benepe, David B.
General Dynamics Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."February 1983"--Cover."General Dynamics."Includes bibliographical references.Mo...

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

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...

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...

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...

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

Abstract

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

Abstract

Extracted data

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