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

Effect of a load-alleviating structure on the landing behavior of a reentry-capsule model /

Hoffman, Edward L.
McGehee, John R.
Stubbs, Sandy M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

Effect of afterbody ejection configurations on the performance at transonic speeds of a pylon-supported Nacelle model having a hot-jet exhaust /

Swihart, John M.
Norton, Harry T.
Mercer, Charles E.
United States. National Aeronautics and Space Administration.

Cover title." October 1962."Aircraft; Propulsion system elements; Propulsion systems, air-jet.Includ...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Margason, Richard J.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

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 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

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

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

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...

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...

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

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 a load-alleviating structure on the landing behavior of a reentry-capsule model /

Hoffman, Edward L.
McGehee, John R.
Stubbs, Sandy M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

Effect of afterbody ejection configurations on the performance at transonic speeds of a pylon-supported Nacelle model having a hot-jet exhaust /

Swihart, John M.
Norton, Harry T.
Mercer, Charles E.
United States. National Aeronautics and Space Administration.

Cover title." October 1962."Aircraft; Propulsion system elements; Propulsion systems, air-jet.Includ...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Margason, Richard J.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

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 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

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

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

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...

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...

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

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 a load-alleviating structure on the landing behavior of a reentry-capsule model /

Hoffman, Edward L.
McGehee, John R.
Stubbs, Sandy M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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