Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35©� swept-wing model and an unswept-wing model /

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).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 /

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

January 1953

" January 27, 1953."Includes bibliographical references (p. 13).Mode of access: Internet

Large-scale wind-tunnel tests and evaluation of the low-speed performance of a 35 degree sweptback wing jet transport model equipped with a blowing boundary-layer-control flap and leading edge slat /

Hickey, David H.
Aoyagi, Kiyoshi.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft.Includes bibliographical references.Mode of access...

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

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 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

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

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

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust /

Tolhurst, William H.
Aoyagi, Kiyoshi.
Ames Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 9).Mode of access: Internet

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 ...

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

Wind-tunnel investigation of the static and dynamic-rotary stability derivatives of a flat-top wing-body model at Mach numbers of 2.5, 3.0 and 3.5 /

Lampkin, Bedford A.
Endicott, Kenneth C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"Ames Research Center, Moffett Field, Calif.""April 1960."Cover title.Includes bibliographical refer...

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

Parks, James H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).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 /

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

January 1953

" January 27, 1953."Includes bibliographical references (p. 13).Mode of access: Internet

Large-scale wind-tunnel tests and evaluation of the low-speed performance of a 35 degree sweptback wing jet transport model equipped with a blowing boundary-layer-control flap and leading edge slat /

Hickey, David H.
Aoyagi, Kiyoshi.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft.Includes bibliographical references.Mode of access...

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

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 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

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

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

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust /

Tolhurst, William H.
Aoyagi, Kiyoshi.
Ames Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 9).Mode of access: Internet

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 ...

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

Wind-tunnel investigation of the static and dynamic-rotary stability derivatives of a flat-top wing-body model at Mach numbers of 2.5, 3.0 and 3.5 /

Lampkin, Bedford A.
Endicott, Kenneth C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"Ames Research Center, Moffett Field, Calif.""April 1960."Cover title.Includes bibliographical refer...

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

Parks, James H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).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 /

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

January 1953

" January 27, 1953."Includes bibliographical references (p. 13).Mode of access: Internet

Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35©� swept-wing model and an unswept-wing model /

Abstract

Extracted data

Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35©� swept-wing model and an unswept-wing model /

Abstract

Extracted data

Related items

Related items