Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

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...

Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds /

Boltz, Frederick W.
Allen, Clyde Q.
Kenyon, George C.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Fluid mechanics.Includes bibliographical referenc...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

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

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

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...

Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid m...

Effects of leading-edge bluntness on flutter characteristics of some square-planform double-wedge airfoils at a Mach number of 15.4 /

Goetz, Robert C.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

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

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...

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...

Radiation emission effects of the equilibrium boundary layer in the stagnation region /

Howe, John Thomas.
United States. National Aeronautics and Space Administration.

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

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...

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...

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

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...

Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds /

Boltz, Frederick W.
Allen, Clyde Q.
Kenyon, George C.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Fluid mechanics.Includes bibliographical referenc...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

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

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

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...

Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid m...

Effects of leading-edge bluntness on flutter characteristics of some square-planform double-wedge airfoils at a Mach number of 15.4 /

Goetz, Robert C.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

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

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...

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...

Radiation emission effects of the equilibrium boundary layer in the stagnation region /

Howe, John Thomas.
United States. National Aeronautics and Space Administration.

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

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...

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...

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

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...

Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds /

Boltz, Frederick W.
Allen, Clyde Q.
Kenyon, George C.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Fluid mechanics.Includes bibliographical referenc...

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Abstract

Extracted data

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Abstract

Extracted data

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