Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes bibliographical references.Mode of access:...

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1975

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

Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models /

Bare, E. Ann.
Capone, Francis J.
Berrier, Bobby L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Planform effects on the supersonic aerodynamics of multibody configurations /

McMillin, S. Naomi (Susan Naomi)
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 1...

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5 /

Powers, Sheryll Goecke.
Ames Research Center.

January 1988

Prepared at Ames Research Center."February 1988"--Cover.Includes bibliographical references (p. 6).M...

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9 /

Bernot, Peter T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"January 1983"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Multiscale turbulence effects in supersonic jets exhausting into still air /

Abdol-Hamid, Khaled S. (Khaled Sayed), 1957-
Wilmoth, Richard G.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 11).M...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds /

Pendergraft, Odis C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

"November 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Effects of curved approach paths and advanced displays on pilot scan patterns /

Harris, Randall L.
Mixon, Randolph W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes bibliographical references.Mode of access:...

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1975

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

Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models /

Bare, E. Ann.
Capone, Francis J.
Berrier, Bobby L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Planform effects on the supersonic aerodynamics of multibody configurations /

McMillin, S. Naomi (Susan Naomi)
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 1...

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5 /

Powers, Sheryll Goecke.
Ames Research Center.

January 1988

Prepared at Ames Research Center."February 1988"--Cover.Includes bibliographical references (p. 6).M...

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9 /

Bernot, Peter T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"January 1983"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Multiscale turbulence effects in supersonic jets exhausting into still air /

Abdol-Hamid, Khaled S. (Khaled Sayed), 1957-
Wilmoth, Richard G.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 11).M...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds /

Pendergraft, Odis C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

"November 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Effects of curved approach paths and advanced displays on pilot scan patterns /

Harris, Randall L.
Mixon, Randolph W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes bibliographical references.Mode of access:...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Abstract

Extracted data

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Abstract

Extracted data

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