Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /

Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Effect of a variable camber and twist wing at transonic Mach numbers /

Ferris, James C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Distributed to depository libraries in microfiche.Subject category 02."December 1984"--Cover.Include...

Wing planform effects at supersonic speeds for an advanced fighter configuration /

Wood, Richard M.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"March 1984"--Cover.Distributed to depository libraries in microfiche.Subject category 02.Includes b...

The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 /

Henderson, William P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

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

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

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

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /

Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Effect of a variable camber and twist wing at transonic Mach numbers /

Ferris, James C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Distributed to depository libraries in microfiche.Subject category 02."December 1984"--Cover.Include...

Wing planform effects at supersonic speeds for an advanced fighter configuration /

Wood, Richard M.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"March 1984"--Cover.Distributed to depository libraries in microfiche.Subject category 02.Includes b...

The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 /

Henderson, William P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

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

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

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

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /

Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Abstract

Extracted data

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Abstract

Extracted data

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