Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45©� sweptback wing of aspect ratio 4 /

Spreemann, Kenneth P.
Alford, William J.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

January 1957

"April 1957."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).Mode of access: Internet

An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included /

Carmel, Melvin M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19,1954."Includes bibliographical references (p. 11).Mode of access: Internet

An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45©� sweptback wing-body configuration at transonic speeds /

Williams, Claude V.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"Declassified September 17, 1958.""October 12, 1954."Cover title.Includes bibliographical references...

Transonic wind-tunnel investigation of the interference between a 45©� sweptback wing and a systematic series of four bodies /

Loving, Donald L.
Wornom, Dewey E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 20, 1952; Declassified October 18, 1956."Includes bibliographical references (p. 14).Mode ...

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

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

January 1953

"Janauary 6, 1953."Includes bibliographical references (p. 11).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45©� sweptback wing /

Bingham, Gene J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"September 28, 1955."Includes bibliographical references (p. 16).Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

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

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

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

Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45©� sweptback wing of aspect ratio 4 and a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96 /

Jacobsen, Carl R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 21, 1953."Includes bibliographical references (p. 8-9).Mode of access: Internet

Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series /

Fournier, Paul G.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 9, 1953."Includes bibliographical references (p. 9).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...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45©� sweptback wing of aspect ratio 4 /

Spreemann, Kenneth P.
Alford, William J.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

January 1957

"April 1957."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).Mode of access: Internet

An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included /

Carmel, Melvin M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19,1954."Includes bibliographical references (p. 11).Mode of access: Internet

An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45©� sweptback wing-body configuration at transonic speeds /

Williams, Claude V.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"Declassified September 17, 1958.""October 12, 1954."Cover title.Includes bibliographical references...

Transonic wind-tunnel investigation of the interference between a 45©� sweptback wing and a systematic series of four bodies /

Loving, Donald L.
Wornom, Dewey E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 20, 1952; Declassified October 18, 1956."Includes bibliographical references (p. 14).Mode ...

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

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

January 1953

"Janauary 6, 1953."Includes bibliographical references (p. 11).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45©� sweptback wing /

Bingham, Gene J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"September 28, 1955."Includes bibliographical references (p. 16).Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

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

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

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

Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45©� sweptback wing of aspect ratio 4 and a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96 /

Jacobsen, Carl R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 21, 1953."Includes bibliographical references (p. 8-9).Mode of access: Internet

Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series /

Fournier, Paul G.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 9, 1953."Includes bibliographical references (p. 9).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...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45©� sweptback wing of aspect ratio 4 /

Spreemann, Kenneth P.
Alford, William J.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

January 1957

"April 1957."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).Mode of access: Internet

Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

Abstract

Extracted data

Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

Abstract

Extracted data

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