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

Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing /

Dickinson, Stanley O.
Hodder, Brent K.
Hall, Leo P.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-18558.Cover title.Includes bibliographical references (p. 7).Mo...

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...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails /

Lockwood, Vernard E.
Thompson, Wilson E.
Langley Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing /

Ray, Edward J.
Taylor, Robert T., NASA researcher.
Langley Research Center.

January 1967

"NASA TM X-1386.""Langley Research Center, Langley Station, Hampton, Va.""June 1967"--Cover.Includes...

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /

Freeman, Delma C., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N69-10733.Includes bibliographical references (p. 15).Mode...

Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications /

Fournier, Roger H.
Langley Research Center.

January 1966

"NASA TM X-1247.""Langley Research Center, Langley Station, Hampton, Va.""August 1966"--Cover.Includ...

NASA research on materials applicable to supersonic transports /

Hardrath, Herbert F.
Heimerl, George J.
Langley Research Center.

January 1964

"NASA TM X-1013"--Cover."Langley Research Center, Langley Station, Hampton Va."--Cover."October 1964...

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

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

Aerodynamic characteristics of a large-scale V/STOL transport model with left and lift-cruise fans /

Hall, Leo P.
Kirk, Jerry V.
Hickey, David H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /

Corlett, William A.
Langley Research Center.

January 1965

"NASA TM X-1151"--Cover."Langley Research Center, Langley Research Center, Hampton, Va."--Cover."Aug...

Transonic aerodynamic damping and oscillatory stability in yaw and pitch for a model of a variable-sweep supersonic transport airplane /

Wright, Bruce R.
Averett, Benjamin T.
United States. National Aeronautics and Space Administration.

"March 1966."Cover title.Includes bibliographical reference (p. 12).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...

Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing /

Dickinson, Stanley O.
Hodder, Brent K.
Hall, Leo P.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-18558.Cover title.Includes bibliographical references (p. 7).Mo...

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...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails /

Lockwood, Vernard E.
Thompson, Wilson E.
Langley Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing /

Ray, Edward J.
Taylor, Robert T., NASA researcher.
Langley Research Center.

January 1967

"NASA TM X-1386.""Langley Research Center, Langley Station, Hampton, Va.""June 1967"--Cover.Includes...

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /

Freeman, Delma C., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N69-10733.Includes bibliographical references (p. 15).Mode...

Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications /

Fournier, Roger H.
Langley Research Center.

January 1966

"NASA TM X-1247.""Langley Research Center, Langley Station, Hampton, Va.""August 1966"--Cover.Includ...

NASA research on materials applicable to supersonic transports /

Hardrath, Herbert F.
Heimerl, George J.
Langley Research Center.

January 1964

"NASA TM X-1013"--Cover."Langley Research Center, Langley Station, Hampton Va."--Cover."October 1964...

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

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

Aerodynamic characteristics of a large-scale V/STOL transport model with left and lift-cruise fans /

Hall, Leo P.
Kirk, Jerry V.
Hickey, David H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /

Corlett, William A.
Langley Research Center.

January 1965

"NASA TM X-1151"--Cover."Langley Research Center, Langley Research Center, Hampton, Va."--Cover."Aug...

Transonic aerodynamic damping and oscillatory stability in yaw and pitch for a model of a variable-sweep supersonic transport airplane /

Wright, Bruce R.
Averett, Benjamin T.
United States. National Aeronautics and Space Administration.

"March 1966."Cover title.Includes bibliographical reference (p. 12).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...

Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing /

Dickinson, Stanley O.
Hodder, Brent K.
Hall, Leo P.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-18558.Cover title.Includes bibliographical references (p. 7).Mo...

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...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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