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

Cascade tests of serrated leading edge blading at high subsonic speeds /

Smith, E. G.
Sowers, H. D.
Ames Research Center.
General Electric Company.

January 1974

"Prepared by General Electric Company ... for Ames Research Center."Cover title.Includes bibliograph...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Effects of shock impingement and other factors on leading-edge heat transfer /

Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 10-11).Mode of access: Internet

Some aerodynamic effects of blunting a projectile nose /

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

"RDT & E Project No. 1M523801A287.""September 1964."Includes bibliographical references (page 22).Mo...

Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 /

Siler, L. G., author.
Deskins, H. E., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"November 1964."Includes bibliographic references (page 5).Report prepared by ARO, Inc., under Air F...

Altitude-velocity table and charts for imperfect air.

Lewis, Clark H. (Clark Houston), 1929-. author.
Burgess, E. G., III., author.
ARO, inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62405334, Task 895303.""November 1965."Includes bibliographical references (page 3)...

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Note on shock reflection coefficient /

Gerber, Nathan.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT&E Project No. 1P222901A201.""August 1966."Includes bibliographical references (page 15).Mode of...

An investigation of spray velocity resulting from high-velocity penetration of thin plates by disks /

Di Battista, John D.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

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...

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

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

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

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Effect of low-velocity or ballistic impact damage on the strength of thin composite and aluminum shear panels /

Farley, Gary L.
United States. Army Aviation Systems Command. Structures Laboratory.

January 1985

Prepared at the U.S. Army Aviation Systems Command's Structures Laboratory."May 1985"--Cover.Include...

Cascade tests of serrated leading edge blading at high subsonic speeds /

Smith, E. G.
Sowers, H. D.
Ames Research Center.
General Electric Company.

January 1974

"Prepared by General Electric Company ... for Ames Research Center."Cover title.Includes bibliograph...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Effects of shock impingement and other factors on leading-edge heat transfer /

Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 10-11).Mode of access: Internet

Some aerodynamic effects of blunting a projectile nose /

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

"RDT & E Project No. 1M523801A287.""September 1964."Includes bibliographical references (page 22).Mo...

Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 /

Siler, L. G., author.
Deskins, H. E., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"November 1964."Includes bibliographic references (page 5).Report prepared by ARO, Inc., under Air F...

Altitude-velocity table and charts for imperfect air.

Lewis, Clark H. (Clark Houston), 1929-. author.
Burgess, E. G., III., author.
ARO, inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62405334, Task 895303.""November 1965."Includes bibliographical references (page 3)...

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Note on shock reflection coefficient /

Gerber, Nathan.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT&E Project No. 1P222901A201.""August 1966."Includes bibliographical references (page 15).Mode of...

An investigation of spray velocity resulting from high-velocity penetration of thin plates by disks /

Di Battista, John D.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

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...

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

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

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

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Effect of low-velocity or ballistic impact damage on the strength of thin composite and aluminum shear panels /

Farley, Gary L.
United States. Army Aviation Systems Command. Structures Laboratory.

January 1985

Prepared at the U.S. Army Aviation Systems Command's Structures Laboratory."May 1985"--Cover.Include...

Cascade tests of serrated leading edge blading at high subsonic speeds /

Smith, E. G.
Sowers, H. D.
Ames Research Center.
General Electric Company.

January 1974

"Prepared by General Electric Company ... for Ames Research Center."Cover title.Includes bibliograph...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

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

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

Abstract

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