Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50⁰ to 74⁰ delta wings on common fuselage /

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50 deg to 74 deg Delta wings on common fuselage

Frink, N. T.
Johnson, T. D., Jr.
Huffman, J. K.

December 1983

Positions of the primary vortex flow reattachment line and longitudinal aerodynamic data were obtain...

Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing /

Quinto, P. Frank.
Paulson, John W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /

Covell, Peter F.
Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."April 1987"--Cover.Includes bibliographical references (p. 6-7)...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

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

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing /

Fink, Marvin P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N 69-17312.Cover title.Includes bibliographical references (p. 1...

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

Dunning, Robert W.
Smith, Fred M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1959

"June 11, 1953; Declassified August 26, 1959."Includes bibliographical references (p. 6).Mode of acc...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds /

Wood, Richard M.
Wesselmann, Gary F.
Byrd, James E.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50 deg to 74 deg Delta wings on common fuselage

Frink, N. T.
Johnson, T. D., Jr.
Huffman, J. K.

December 1983

Positions of the primary vortex flow reattachment line and longitudinal aerodynamic data were obtain...

Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing /

Quinto, P. Frank.
Paulson, John W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /

Covell, Peter F.
Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."April 1987"--Cover.Includes bibliographical references (p. 6-7)...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

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

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing /

Fink, Marvin P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N 69-17312.Cover title.Includes bibliographical references (p. 1...

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

Dunning, Robert W.
Smith, Fred M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1959

"June 11, 1953; Declassified August 26, 1959."Includes bibliographical references (p. 6).Mode of acc...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds /

Wood, Richard M.
Wesselmann, Gary F.
Byrd, James E.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50⁰ to 74⁰ delta wings on common fuselage /

Abstract

Extracted data

Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50⁰ to 74⁰ delta wings on common fuselage /

Abstract

Extracted data

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