Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° /

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

West, F. E.
United States. National Aeronautics and Space Administration.

Cover title." November 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and l...

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

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

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

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

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

Foster, Gerald V.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75° /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Aerodynamic characteristics of a 60° sweptback-wing airplane configuration having tail surfaces located outboard of the wingtips at mach numbers of 2.30, 2.97, 3.51, and 4.06 /

Sleeman, Jr., William C.
Fournier, Roger H.
Church, James D.
Langley Research Center.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

West, F. E.
United States. National Aeronautics and Space Administration.

Cover title." November 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and l...

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

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

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

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

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

Foster, Gerald V.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75° /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Aerodynamic characteristics of a 60° sweptback-wing airplane configuration having tail surfaces located outboard of the wingtips at mach numbers of 2.30, 2.97, 3.51, and 4.06 /

Sleeman, Jr., William C.
Fournier, Roger H.
Church, James D.
Langley Research Center.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

West, F. E.
United States. National Aeronautics and Space Administration.

Cover title." November 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and l...

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

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

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

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

Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° /

Abstract

Extracted data

Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° /

Abstract

Extracted data

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