Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies /

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical tables."July 1963."Cover title.Includes bibl...

Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at Mach number from 1.57 to 2.86 /

Fuller, Dennis E.
Langhans, Victor E.
United States. National Aeronautics and Space Administration.

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

Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 /

Lockwood, Vernard E.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-170.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Investigation of the normal-force, axial-force, and pitching-moment characteristics of blunt low-fineness-ratio bodies of revolution at a mach number of 3.55 /

McDearmon, Russell W.
Lawson, Warren A
United States. National Aeronautics and Space Administration.

January 1961

"April 1961."Includes bibliographical references (p. 14-15).Mode of access: Internet

Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /

Canning, Thomas N.
Ames Research Center.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19, 1954."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

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...

Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile /

Schult, Eugene D.
Langley Research Center.

January 1960

"NASA TN D-205.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includ...

Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings /

Widmayer, E.
Clevenston, S. A.
Lauten, W. T.
Langley Research Center.

January 1960

"NASA TN D-229.""Langley Research Center, Langley Field, Va.""April 1960."Cover title.Includes bibli...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 /

Robinson, Ross B.
Langley Research Center.

January 1959

"NASA TN D-37.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Mode o...

Lift generation on a circular cylinder by tangential blowing from surface slots /

Lockwood, Vernard E.
Langley Research Center.

January 1960

"NASA TN D-244.""Langley Research Center, Langley Field, Va.""May 1960."Cover title.Includes bibliog...

Experimentally determined local flow properties and drag coefficients for a family of blunt bodies at mach numbers from 2.49 to 4.63 [electronic resource[ /

Stallings, Robert L. Jr.
United States. National Aeronautics and Space Administration.

"October 1967 ."Includes bibliographical references.Mode of access: Internet.Mode of access: World W...

Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane /

Tambor, Ronald.
Flight Research Center (U.S.)

January 1960

"NASA TN D-30.""Flight Research Center, Edwards, Calif.""September 1960."Title from cover.Includes b...

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical tables."July 1963."Cover title.Includes bibl...

Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at Mach number from 1.57 to 2.86 /

Fuller, Dennis E.
Langhans, Victor E.
United States. National Aeronautics and Space Administration.

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

Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 /

Lockwood, Vernard E.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-170.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Investigation of the normal-force, axial-force, and pitching-moment characteristics of blunt low-fineness-ratio bodies of revolution at a mach number of 3.55 /

McDearmon, Russell W.
Lawson, Warren A
United States. National Aeronautics and Space Administration.

January 1961

"April 1961."Includes bibliographical references (p. 14-15).Mode of access: Internet

Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /

Canning, Thomas N.
Ames Research Center.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19, 1954."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

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...

Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile /

Schult, Eugene D.
Langley Research Center.

January 1960

"NASA TN D-205.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includ...

Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings /

Widmayer, E.
Clevenston, S. A.
Lauten, W. T.
Langley Research Center.

January 1960

"NASA TN D-229.""Langley Research Center, Langley Field, Va.""April 1960."Cover title.Includes bibli...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 /

Robinson, Ross B.
Langley Research Center.

January 1959

"NASA TN D-37.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Mode o...

Lift generation on a circular cylinder by tangential blowing from surface slots /

Lockwood, Vernard E.
Langley Research Center.

January 1960

"NASA TN D-244.""Langley Research Center, Langley Field, Va.""May 1960."Cover title.Includes bibliog...

Experimentally determined local flow properties and drag coefficients for a family of blunt bodies at mach numbers from 2.49 to 4.63 [electronic resource[ /

Stallings, Robert L. Jr.
United States. National Aeronautics and Space Administration.

"October 1967 ."Includes bibliographical references.Mode of access: Internet.Mode of access: World W...

Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane /

Tambor, Ronald.
Flight Research Center (U.S.)

January 1960

"NASA TN D-30.""Flight Research Center, Edwards, Calif.""September 1960."Title from cover.Includes b...

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical tables."July 1963."Cover title.Includes bibl...

Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at Mach number from 1.57 to 2.86 /

Fuller, Dennis E.
Langhans, Victor E.
United States. National Aeronautics and Space Administration.

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

Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies /

Abstract

Extracted data

Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies /

Abstract

Extracted data

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