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° /

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° /

Robinson, Ross B.
Howard, Paul W.
Langley Research Center.

January 1960

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

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

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 /

Robinson, Ross B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 28, 1952."Includes bibliographical references (p. 7-8).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

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

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

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 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

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).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

Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Sevier, John R.
United States. National Aeronautics and Space Administration.

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

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

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° /

Robinson, Ross B.
Howard, Paul W.
Langley Research Center.

January 1960

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

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

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 /

Robinson, Ross B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 28, 1952."Includes bibliographical references (p. 7-8).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

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

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

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 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

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).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

Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Sevier, John R.
United States. National Aeronautics and Space Administration.

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

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

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° /

Robinson, Ross B.
Howard, Paul W.
Langley Research Center.

January 1960

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

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

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 /

Robinson, Ross B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 28, 1952."Includes bibliographical references (p. 7-8).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° /

Abstract

Extracted data

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° /

Abstract

Extracted data

Related items

Related items