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 /

High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails /

Lockwood, Vernard E.
Langley Research Center.

January 1966

"NASA TM X-1199.""Langley Research Center, Langley Station, Hampton, Va.""March 1966"--Cover.Include...

Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 /

Kempel, Robert W.
Manke, John A.
United States. National Aeronautics and Space Administration.

January 1974

"January 1974."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Tables and charts for estimating stall effects on lifting-rotor characteristics /

Gessow, Alfred.
Tapscott, Robert J.
Langley Research Center.

January 1960

"NASA TN D-243.""Langley Research Center, Langley Field, Va.""May 1960."Cover title.Includes bibliog...

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

Letko, William.
Langley Research Center.

January 1960

"NASA TN D-226.""Langley Research Center, Langley Field, Va..""April 1960."Cover title.Includes bibl...

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

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...

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

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...

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers /

Strutz, Larry W.
Flight Research Center (U.S.)

January 1972

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 18.Mode of access: Internet

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

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...

Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /

Brooks, Eugene N.
Blackwell, James A.
Decker, John P.
Langley Research Center.

January 1967

"NASA TM X-1345.""Langley Research Center, Langley Station, Hampton, Va.""February 1967"--Cover.Incl...

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...

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...

High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails /

Lockwood, Vernard E.
Langley Research Center.

January 1966

"NASA TM X-1199.""Langley Research Center, Langley Station, Hampton, Va.""March 1966"--Cover.Include...

Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 /

Kempel, Robert W.
Manke, John A.
United States. National Aeronautics and Space Administration.

January 1974

"January 1974."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Tables and charts for estimating stall effects on lifting-rotor characteristics /

Gessow, Alfred.
Tapscott, Robert J.
Langley Research Center.

January 1960

"NASA TN D-243.""Langley Research Center, Langley Field, Va.""May 1960."Cover title.Includes bibliog...

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

Letko, William.
Langley Research Center.

January 1960

"NASA TN D-226.""Langley Research Center, Langley Field, Va..""April 1960."Cover title.Includes bibl...

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

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...

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

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...

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers /

Strutz, Larry W.
Flight Research Center (U.S.)

January 1972

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 18.Mode of access: Internet

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

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...

Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /

Brooks, Eugene N.
Blackwell, James A.
Decker, John P.
Langley Research Center.

January 1967

"NASA TM X-1345.""Langley Research Center, Langley Station, Hampton, Va.""February 1967"--Cover.Incl...

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...

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...

High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails /

Lockwood, Vernard E.
Langley Research Center.

January 1966

"NASA TM X-1199.""Langley Research Center, Langley Station, Hampton, Va.""March 1966"--Cover.Include...

Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 /

Kempel, Robert W.
Manke, John A.
United States. National Aeronautics and Space Administration.

January 1974

"January 1974."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Tables and charts for estimating stall effects on lifting-rotor characteristics /

Gessow, Alfred.
Tapscott, Robert J.
Langley Research Center.

January 1960

"NASA TN D-243.""Langley Research Center, Langley Field, Va.""May 1960."Cover title.Includes bibliog...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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