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

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 (...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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

Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios /

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

January 1968

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

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 circulation plan-form aircraft with a peripheral jet for lift, thrust, and control / Richard K. Grief and William H.Tolhurst Jr.

Grief, Richard K.
Tolhurst, William H.
United States. National Aeronautics and Space Administration.

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

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 tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps /

Weiberg, James A.
Page, V. Robert.
Ames Research Center.

January 1959

"NASA TN D-25.""Ames Research Center, Moffett Field, Calif.""September 1959."Title from cover.Includ...

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 tests of a 1/20-scale airship model with stern propellers /

McLemore, H. Clyde.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Stability and control;Includes bibliographical re...

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

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...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

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

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...

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 (...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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

Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios /

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

January 1968

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

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 circulation plan-form aircraft with a peripheral jet for lift, thrust, and control / Richard K. Grief and William H.Tolhurst Jr.

Grief, Richard K.
Tolhurst, William H.
United States. National Aeronautics and Space Administration.

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

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 tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps /

Weiberg, James A.
Page, V. Robert.
Ames Research Center.

January 1959

"NASA TN D-25.""Ames Research Center, Moffett Field, Calif.""September 1959."Title from cover.Includ...

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 tests of a 1/20-scale airship model with stern propellers /

McLemore, H. Clyde.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Stability and control;Includes bibliographical re...

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

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...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

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

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...

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 (...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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

Abstract

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

Abstract

Extracted data

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