Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport /

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /

Freeman, Delma C., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N69-10733.Includes bibliographical references (p. 15).Mode...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Large-scale wind-tunnel investigation of a V/STOL transport model with wing-mounted lift fans and fuselage-mounted life-cruise engines for propulsion /

Kirk, Jerry V.
Hall, Leo P.
Hodder, Brent K.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

Prepared by Ames Research Center."N67-40198."Includes bibliographical references (p. 10).Mode of acc...

Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Shaw, David S.
Henderson, William P.
Langley Research Center.

Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing /

Freeman, Delma C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-18250.Includes bibliographical references (p. 17).Mode...

Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

Winston, Matthew M.
Huston, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N69-28097.Cover title.Includes bibliographical references (p. 9)...

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust /

Tolhurst, William H.
Aoyagi, Kiyoshi.
Ames Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 9).Mode of access: Internet

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.Mode of access: Internet

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /

Freeman, Delma C., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N69-10733.Includes bibliographical references (p. 15).Mode...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Large-scale wind-tunnel investigation of a V/STOL transport model with wing-mounted lift fans and fuselage-mounted life-cruise engines for propulsion /

Kirk, Jerry V.
Hall, Leo P.
Hodder, Brent K.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

Prepared by Ames Research Center."N67-40198."Includes bibliographical references (p. 10).Mode of acc...

Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Shaw, David S.
Henderson, William P.
Langley Research Center.

Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing /

Freeman, Delma C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-18250.Includes bibliographical references (p. 17).Mode...

Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

Winston, Matthew M.
Huston, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N69-28097.Cover title.Includes bibliographical references (p. 9)...

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust /

Tolhurst, William H.
Aoyagi, Kiyoshi.
Ames Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 9).Mode of access: Internet

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.Mode of access: Internet

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport /

Abstract

Extracted data

Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport /

Abstract

Extracted data

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