An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen.

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...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

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

Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust /

McFarland, Donald R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Fluid mechanics; Stability and control.Includes bib...

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Subsonic longitudinal aerodynamic characteristics of disks with elliptic cross sections and thickness-diameter rations from 0.225 to 0.425 /

Demele, Fred A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Stability and control;Includes b...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

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

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ /

Penland, Jim A.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles;Includes bibliographical reference...

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...

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 /

Czarnecki, K. R.
Monta, William J.
United States. National Aeronautics and Space Administration.

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

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

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...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

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

Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust /

McFarland, Donald R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Fluid mechanics; Stability and control.Includes bib...

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Subsonic longitudinal aerodynamic characteristics of disks with elliptic cross sections and thickness-diameter rations from 0.225 to 0.425 /

Demele, Fred A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Stability and control;Includes b...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

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

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ /

Penland, Jim A.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles;Includes bibliographical reference...

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...

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 /

Czarnecki, K. R.
Monta, William J.
United States. National Aeronautics and Space Administration.

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

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

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...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

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

An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen.

Abstract

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An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen.

Abstract

Extracted data

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