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Some aerodynamic effects of blunting a projectile nose /

Dickinson, Elizabeth R.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

Abstract

"RDT & E Project No. 1M523801A287.""September 1964."Includes bibliographical references (page 22).Mode of access: Internet

Extracted data

Related items

Local heat transfer to blunt noses at high supersonic speeds /

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Langley Aeronautical Laboratory.
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An investigation of the effects of shock impingement on a blunt leading edge /

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Palko, R. L., author.
ARO, Inc. sponsor.
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Langley Aeronautical Laboratory.
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Foster, A. D., compiler.
U.S. Atomic Energy Commission.
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"SC-R-64-1312 is a classified supplement to this monograph.""January 1965."At head of title: SC-R-64...

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Langley Research Center.

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Langley Aeronautical Laboratory.
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January 1957

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An investigation of the effects of shock impingement on a blunt leading edge /

Ray, A. D., author.
Palko, R. L., author.
ARO, Inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62495334, Task 136607.""July 1965."Includes bibliographical references (page 6).Air...

Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Wehrend, William R.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

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...

Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ /

Brooks, Cuyler W.
Trescot, Charles D.
United States. National Aeronautics and Space Administration.

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

The effect of nose radius and shape of the aerodynamic characteristics of a fuselage and a wing-fuselage combination at angles of attack /

Gapcynski, John P.
Robins, A. Warner.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"October 22, 1953."Includes bibliographical references (p. 10-11).Mode of access: Internet

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...

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...

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

Effect of centerbody boundary-layer removal near the throat of three conical nose inlets at mach 1.6 to 2.0 /

Kremzier, Emil J.
Wise, George A.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"November 15, 1955."Includes bibliographical references (p. 7-8).Mode of access: Internet

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...

A compilation of longitudinal aerodynamic characteristics including pressure information for sharp-and blunt-nose cones having flat and modified bases /

Foster, A. D., compiler.
U.S. Atomic Energy Commission.
Sandia Corporation.

January 1965

"SC-R-64-1312 is a classified supplement to this monograph.""January 1965."At head of title: SC-R-64...

A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a Mach number of 6.0 /

Ashby, George C.
Cary, Aubrey M.
Langley Research Center.

Prepared at Langley Research Center."June 1965"--Cover.Includes bibliographical references (p. 14-15...

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...

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

Local heat transfer to blunt noses at high supersonic speeds /

Stoney, William E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"July 12, 1957."Includes bibliographical references (p. 7-8).Mode of access: Internet

An investigation of the effects of shock impingement on a blunt leading edge /

Ray, A. D., author.
Palko, R. L., author.
ARO, Inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62495334, Task 136607.""July 1965."Includes bibliographical references (page 6).Air...

Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Wehrend, William R.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...