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

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

Full scale wind-tunnel tests of blowing boundary-layer control applied to a helicopter rotor /

McCloud, John L.
Brady, James A.
Hall, Leo P.
United States. National Aeronautics and Space Administration.

Cover title." September 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical referen...

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)...

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Large-scale wind-tunnel tests of a wingless vertical take-off and landing aircraft - preliminary results. /

Koenig, David G.
Brady, James A.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

A large-scale wind-tunnel investigation of a wingless vertical take-off and landing aircraft /

Koenig, David G.
Brady, James. A
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane /

Dickinson, Stanley O.
Deckert, W. H. (Wallace H.)
Page, V. Robert.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 7).Mode of access: Internet

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...

Large-scale wind-tunnel tests of an airplane model with two propellers and rotaing cylinder flaps /

Weiberg, James A.
Gamse, Berl.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 9).Mode of access: Internet

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

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 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 the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

Yaggy, Paul F.
Mort, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

Full scale wind-tunnel tests of blowing boundary-layer control applied to a helicopter rotor /

McCloud, John L.
Brady, James A.
Hall, Leo P.
United States. National Aeronautics and Space Administration.

Cover title." September 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical referen...

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)...

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Large-scale wind-tunnel tests of a wingless vertical take-off and landing aircraft - preliminary results. /

Koenig, David G.
Brady, James A.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

A large-scale wind-tunnel investigation of a wingless vertical take-off and landing aircraft /

Koenig, David G.
Brady, James. A
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane /

Dickinson, Stanley O.
Deckert, W. H. (Wallace H.)
Page, V. Robert.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 7).Mode of access: Internet

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...

Large-scale wind-tunnel tests of an airplane model with two propellers and rotaing cylinder flaps /

Weiberg, James A.
Gamse, Berl.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 9).Mode of access: Internet

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

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 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 the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

Yaggy, Paul F.
Mort, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

Full scale wind-tunnel tests of blowing boundary-layer control applied to a helicopter rotor /

McCloud, John L.
Brady, James A.
Hall, Leo P.
United States. National Aeronautics and Space Administration.

Cover title." September 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical referen...

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)...

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

Abstract

Extracted data

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

Abstract

Extracted data

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