Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle /

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Integration of aft-fuselage-mounted flow-through engine nacelles on an advanced transport configuration at Mach numbers from 0.6 to 1.0 /

Blaha, Bernard J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of...

Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing /

Lee, Edwin E.
Pendergraft, Odis C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 2...

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Pendergraft, Odis C.
Carlson, John R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"November 1987"--Cover.Includes bibliographical references (p. 3).Mode of access: Internet

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Abeyounis, William Kelly.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986."Includes bibliographical references (p. 4).Mode of ...

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...

Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17 scale, twin-engine, low-wing transport model /

Pendergraft, Odis C.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 9).Mode of access: Inter...

An experimental investigation of nacelle-pylon installation on an unswept wing at subsonic and transonic speeds /

Carlson, John R.
Compton, William B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

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

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement /

Henderson, William P.
Abeyounis, William Kelly.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1985

Distributed to depository libraries in microfiche.Chiefly ill."December 1985"--Cover.Bibliography: p...

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Integration of aft-fuselage-mounted flow-through engine nacelles on an advanced transport configuration at Mach numbers from 0.6 to 1.0 /

Blaha, Bernard J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of...

Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing /

Lee, Edwin E.
Pendergraft, Odis C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 2...

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Pendergraft, Odis C.
Carlson, John R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1987

"November 1987"--Cover.Includes bibliographical references (p. 3).Mode of access: Internet

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport /

Lamb, Milton.
Abeyounis, William Kelly.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986."Includes bibliographical references (p. 4).Mode of ...

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...

Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17 scale, twin-engine, low-wing transport model /

Pendergraft, Odis C.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 9).Mode of access: Inter...

An experimental investigation of nacelle-pylon installation on an unswept wing at subsonic and transonic speeds /

Carlson, John R.
Compton, William B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

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

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement /

Henderson, William P.
Abeyounis, William Kelly.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1985

Distributed to depository libraries in microfiche.Chiefly ill."December 1985"--Cover.Bibliography: p...

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Integration of aft-fuselage-mounted flow-through engine nacelles on an advanced transport configuration at Mach numbers from 0.6 to 1.0 /

Blaha, Bernard J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of...

Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle /

Abstract

Extracted data

Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle /

Abstract

Extracted data

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