An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers /

Full-scale wind-tunnel tests of a low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading- and trailing-edge flaps /

Kelly, Mark W.
Maki, Ralph L.
Tolhurst, William H.
Ames Research Center.

January 1959

"NASA TN D-135.""Ames Research Center, Moffett Field, Calif.""September 1959."Title from cover.Inclu...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An examination of methods of buffeting analysis based on experiments with wings of varying stiffness /

Rainey, A. Gerald.
Byrdsong, Thomas A.
Langley Research Center.

January 1959

"NASA TN D-3.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane /

Tambor, Ronald.
Flight Research Center (U.S.)

January 1960

"NASA TN D-30.""Flight Research Center, Edwards, Calif.""September 1960."Title from cover.Includes b...

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Investigation at transonic speeds to determine lateral control effectiveness of blowing laterally over surfaces of 30° and 45° swept wings /

Hammond, Alexander D.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-42.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 /

Demele, Fred A.
Ames Research Center.

January 1959

"NASA TN D-138.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Includ...

Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /

Matranga, Gene J.
Armstrong, Neil, 1930-
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of double slotted flaps on a swept-wing transport model /

Naeseth, Rodger L.
Davenport, Edwin E.
Langley Research Center.

January 1959

"NASA TN D-103.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

Flight investigations of automatic stabilization of an airplane having static longitudinal instability /

Russell, Walter R.
Alford, William L.
Sjoberg, S. A.
Langley Research Center.

January 1959

"NASA TN D-173.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Flight investigation of stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-45.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes /

Riebe, John M.
Langley Research Center.

January 1959

"NASA TN D-19.""Langley Research Center, Langley Field, Va.""September 1959."Cover title.Mode of acc...

Analysis of acceleration, airspeed and gust-velocity data from a four-engine turboprop transport operating over the eastern United States /

Copp, Martin R.
Fetner, Mary W.
Langley Research Center.

January 1959

"NASA TN D-36.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Full-scale wind-tunnel tests of a low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading- and trailing-edge flaps /

Kelly, Mark W.
Maki, Ralph L.
Tolhurst, William H.
Ames Research Center.

January 1959

"NASA TN D-135.""Ames Research Center, Moffett Field, Calif.""September 1959."Title from cover.Inclu...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An examination of methods of buffeting analysis based on experiments with wings of varying stiffness /

Rainey, A. Gerald.
Byrdsong, Thomas A.
Langley Research Center.

January 1959

"NASA TN D-3.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane /

Tambor, Ronald.
Flight Research Center (U.S.)

January 1960

"NASA TN D-30.""Flight Research Center, Edwards, Calif.""September 1960."Title from cover.Includes b...

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Investigation at transonic speeds to determine lateral control effectiveness of blowing laterally over surfaces of 30° and 45° swept wings /

Hammond, Alexander D.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-42.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 /

Demele, Fred A.
Ames Research Center.

January 1959

"NASA TN D-138.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Includ...

Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /

Matranga, Gene J.
Armstrong, Neil, 1930-
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of double slotted flaps on a swept-wing transport model /

Naeseth, Rodger L.
Davenport, Edwin E.
Langley Research Center.

January 1959

"NASA TN D-103.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

Flight investigations of automatic stabilization of an airplane having static longitudinal instability /

Russell, Walter R.
Alford, William L.
Sjoberg, S. A.
Langley Research Center.

January 1959

"NASA TN D-173.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Flight investigation of stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-45.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes /

Riebe, John M.
Langley Research Center.

January 1959

"NASA TN D-19.""Langley Research Center, Langley Field, Va.""September 1959."Cover title.Mode of acc...

Analysis of acceleration, airspeed and gust-velocity data from a four-engine turboprop transport operating over the eastern United States /

Copp, Martin R.
Fetner, Mary W.
Langley Research Center.

January 1959

"NASA TN D-36.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Full-scale wind-tunnel tests of a low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading- and trailing-edge flaps /

Kelly, Mark W.
Maki, Ralph L.
Tolhurst, William H.
Ames Research Center.

January 1959

"NASA TN D-135.""Ames Research Center, Moffett Field, Calif.""September 1959."Title from cover.Inclu...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An examination of methods of buffeting analysis based on experiments with wings of varying stiffness /

Rainey, A. Gerald.
Byrdsong, Thomas A.
Langley Research Center.

January 1959

"NASA TN D-3.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers /

Abstract

Extracted data

An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers /

Abstract

Extracted data

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