Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

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...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

Mutual aerodynamic interference effects for multiple bodies by the cross-flow corrections method /

Martin, Fred W., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Project 2567, Task 02.""June 1971."Includes bibliographical references (page 51).Mode of access: In...

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

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

Mutual aerodynamic interference effects for two axisymmetric bodies /

Martin, Fred W., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"The work described in this report was done during the period from September 1972 through June 1973 ...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

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

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

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Unsteady aerodynamics for advanced configurations.

Rodemich, E. R., author.
Andrew, L. V., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

"May 1965."Includes bibliograpical references (pages 41-42).Print reproduction.Air Force Contract No...

Supplementary note on modified-impact-theory calculations for bodies of revolution having minimum drag at hypersonic speeds /

Resnikoff, Meyer M.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "July 18, 1952."Includes bibliographical references: p. 11.Mode of access: Internet

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

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

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...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

Mutual aerodynamic interference effects for multiple bodies by the cross-flow corrections method /

Martin, Fred W., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Project 2567, Task 02.""June 1971."Includes bibliographical references (page 51).Mode of access: In...

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

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

Mutual aerodynamic interference effects for two axisymmetric bodies /

Martin, Fred W., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"The work described in this report was done during the period from September 1972 through June 1973 ...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

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

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

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Unsteady aerodynamics for advanced configurations.

Rodemich, E. R., author.
Andrew, L. V., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

"May 1965."Includes bibliograpical references (pages 41-42).Print reproduction.Air Force Contract No...

Supplementary note on modified-impact-theory calculations for bodies of revolution having minimum drag at hypersonic speeds /

Resnikoff, Meyer M.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "July 18, 1952."Includes bibliographical references: p. 11.Mode of access: Internet

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

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

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...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Abstract

Extracted data

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Abstract

Extracted data

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