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

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

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

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.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 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...

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...

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

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

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4-5)....

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 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...

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...

An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics /

Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"August 1979"--Cover.Includes bibliographical references.Mode of access: Internet

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...

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

Effect of afterbody terminal fairings on the performance of a pylon-mounted turbojet-nacelle model /

Willis, Conrad M.
Mercer, Charles E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Thrust-reverser flow investigation on a twin-engine transport /

Gatlin, Gregory M. (Gregory Michael)
Quinto, P. Frank.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 17).Mode of access: Internet

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

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

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.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 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...

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...

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

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

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4-5)....

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 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...

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...

An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics /

Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"August 1979"--Cover.Includes bibliographical references.Mode of access: Internet

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...

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

Effect of afterbody terminal fairings on the performance of a pylon-mounted turbojet-nacelle model /

Willis, Conrad M.
Mercer, Charles E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Thrust-reverser flow investigation on a twin-engine transport /

Gatlin, Gregory M. (Gregory Michael)
Quinto, P. Frank.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 17).Mode of access: Internet

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

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

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.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 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...

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items