Research on blunt-faced entry configurations at angles of attack Between 60° and 90° /

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

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

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 /

Robins, A. Warner.

"October 30, 1953. Declassified September 17, 1958"--Cover.Caption title.Includes bibliographical re...

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

The penetration of porous projectiles in aluminum and plastic targets /

Fish, Richard H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

A preliminary investigation of the effect of bumpers as a means of reducing projectile penetration /

Funkhouser, John O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Materials, other; Structures.Includes bibliographical references.Mode of ac...

Angle-of-attack analysis for Project Fire 1 payload reentry flight /

Woodbury, Gerard E.
Langley Research Center.

Prepared at Langley Research Center."April 1966"--Cover.Includes bibliographical references (p. 25)....

A comparison of the performance of four side-mounted inlets over a Mach number range of 0.88 to 2.2 and angles of attack to 14° /

Presley, Leroy L.
Peterson, William P.
Ames Research Center.

January 1960

"January 1960."Caption title.Includes bibliographical references (p. 14-15).Mode of access: Internet

The dependency of penetration on the momentum per unit area of the impacting projectile and the resistance of materials to penetration /

Collins, Rufus Davis, 1932-
Kinard, William H.
Langley Research Center.

Prepared at Langley Research Center."May 1960."Cover title.Includes bibliographical references (p. 1...

Optimum target orientation in nuclear reaction experiments /

Need, John Logan, 1927-
Lewis Research Center.

Prepared at Lewis Research Center."November 1965"--Cover.Includes bibliographical references (p. 24)...

Observations on the flows past blunt bodies at transonic speeds /

Everhart, Philip E.
Lindsey, Walter F.
United States. National Aeronautics and Space Administration.

"1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Evaluation of five conical center-body supersonic diffusers at several angles of attack /

Englert, Gerald W.
Obery, Leonard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 5, 1952."Title from cover.Includes bibliographical references: p. 7.Mode of acc...

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

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

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 /

Robins, A. Warner.

"October 30, 1953. Declassified September 17, 1958"--Cover.Caption title.Includes bibliographical re...

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

The penetration of porous projectiles in aluminum and plastic targets /

Fish, Richard H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

A preliminary investigation of the effect of bumpers as a means of reducing projectile penetration /

Funkhouser, John O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Materials, other; Structures.Includes bibliographical references.Mode of ac...

Angle-of-attack analysis for Project Fire 1 payload reentry flight /

Woodbury, Gerard E.
Langley Research Center.

Prepared at Langley Research Center."April 1966"--Cover.Includes bibliographical references (p. 25)....

A comparison of the performance of four side-mounted inlets over a Mach number range of 0.88 to 2.2 and angles of attack to 14° /

Presley, Leroy L.
Peterson, William P.
Ames Research Center.

January 1960

"January 1960."Caption title.Includes bibliographical references (p. 14-15).Mode of access: Internet

The dependency of penetration on the momentum per unit area of the impacting projectile and the resistance of materials to penetration /

Collins, Rufus Davis, 1932-
Kinard, William H.
Langley Research Center.

Prepared at Langley Research Center."May 1960."Cover title.Includes bibliographical references (p. 1...

Optimum target orientation in nuclear reaction experiments /

Need, John Logan, 1927-
Lewis Research Center.

Prepared at Lewis Research Center."November 1965"--Cover.Includes bibliographical references (p. 24)...

Observations on the flows past blunt bodies at transonic speeds /

Everhart, Philip E.
Lindsey, Walter F.
United States. National Aeronautics and Space Administration.

"1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Evaluation of five conical center-body supersonic diffusers at several angles of attack /

Englert, Gerald W.
Obery, Leonard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 5, 1952."Title from cover.Includes bibliographical references: p. 7.Mode of acc...

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

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

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 /

Robins, A. Warner.

"October 30, 1953. Declassified September 17, 1958"--Cover.Caption title.Includes bibliographical re...

Research on blunt-faced entry configurations at angles of attack Between 60° and 90° /

Abstract

Extracted data

Research on blunt-faced entry configurations at angles of attack Between 60° and 90° /

Abstract

Extracted data

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