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

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).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 ...

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 of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Low-speed wind-tunnel investigation of a wingless jet VTOL transport model /

McKinney, Marion O.
Langley Research Center.

January 1959

"NASA TN D-57.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps /

Yip, Long P.
Langley Research Center.

January 1987

Prepared at Langley Research Center."May 1987"--Cover.Includes bibliographical references (p. 7).Mod...

Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane /

Sandford, Maynard C.
Ruhlin, Charles L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Prepared by Langley Research Center.N 69-16211.Includes bibliographical references (p. 13).Mode of a...

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing /

Byrdsong, Thomas A.
Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche.Chiefly tables."June 1983"--Cover."Supplement to N...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).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 ...

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 of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Low-speed wind-tunnel investigation of a wingless jet VTOL transport model /

McKinney, Marion O.
Langley Research Center.

January 1959

"NASA TN D-57.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps /

Yip, Long P.
Langley Research Center.

January 1987

Prepared at Langley Research Center."May 1987"--Cover.Includes bibliographical references (p. 7).Mod...

Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane /

Sandford, Maynard C.
Ruhlin, Charles L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Prepared by Langley Research Center.N 69-16211.Includes bibliographical references (p. 13).Mode of a...

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing /

Byrdsong, Thomas A.
Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche.Chiefly tables."June 1983"--Cover."Supplement to N...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

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

Abstract

Extracted data

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

Abstract

Extracted data

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