Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

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

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method /

Sleeman, William C.
Morrison, William D.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"December 12, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

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

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

Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99° of a reentry glider having folding wing-tip panels /

Olstad, Walter B.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).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

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

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

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

Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ /

Brooks, Cuyler W.
Trescot, Charles D.
United States. National Aeronautics and Space Administration.

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

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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

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

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

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

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method /

Sleeman, William C.
Morrison, William D.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"December 12, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

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

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

Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99° of a reentry glider having folding wing-tip panels /

Olstad, Walter B.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).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

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

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

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

Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ /

Brooks, Cuyler W.
Trescot, Charles D.
United States. National Aeronautics and Space Administration.

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

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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

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

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

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

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method /

Sleeman, William C.
Morrison, William D.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"December 12, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Abstract

Extracted data

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Abstract

Extracted data

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