Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency /

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...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

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...

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 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...

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

Cover title." April 1962."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles, Stabilit...

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...

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 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...

Secondary flow fields embedded in hypersonic shock layers /

Seiff, Alvin.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stability and con...

A method for calculating the aerodynamic forces due to arbitrary, time dependent downwash for a class of thin, flexible wings at supersonic speeds /

Warner, Robert W.
Packard, Barbara B.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flow, supersonic; Loads, aeroelasticity; Vibration and flutter.Includes ...

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...

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...

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...

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...

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...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

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...

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 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...

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

Cover title." April 1962."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles, Stabilit...

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...

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 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...

Secondary flow fields embedded in hypersonic shock layers /

Seiff, Alvin.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stability and con...

A method for calculating the aerodynamic forces due to arbitrary, time dependent downwash for a class of thin, flexible wings at supersonic speeds /

Warner, Robert W.
Packard, Barbara B.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flow, supersonic; Loads, aeroelasticity; Vibration and flutter.Includes ...

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...

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...

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...

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...

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...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

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...

Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency /

Abstract

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Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency /

Abstract

Extracted data

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