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

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...

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).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

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

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust /

Tolhurst, William H.
Aoyagi, Kiyoshi.
Ames Research Center.

January 1964

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

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

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

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

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

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

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

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

Parks, James H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

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...

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).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

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

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust /

Tolhurst, William H.
Aoyagi, Kiyoshi.
Ames Research Center.

January 1964

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

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

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

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

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

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

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

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

Parks, James H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

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...

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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