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

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds /

Sandahl, Carl A.
Stoney, William E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 18, 1954."Includes bibliographical references (p. 11).Mode of access: Internet

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.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)...

Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 /

Bare, E. Ann.
Haddad, Raymond C.
Reubush, David E.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 26).Mode of access: Inte...

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)....

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...

Comparisons of two-dimensional shock-expansion theory with experimental aerodynamic data for delta-planform wings at high supersonic speeds /

Jernell, Lloyd S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds /

Erickson, Gary E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 20-21).Mode of access: I...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

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 ...

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

McMillin, S. Naomi (Susan Naomi)
Murman, Earll M., 1942-
Thomas, James L. (James Lee), 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 98-99.Mode of access: Internet

Visualization of leading edge vortices on a series of flat plate delta wings /

Payne, Francis M.
Nelson, Robert C., 1942-
Ng, T. Terry.
Ames Research Center.
University of Notre Dame. Dept. of Aerospace and Mechanical Engineering.

January 1991

Prepared at the Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, for Ames Re...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds /

Sandahl, Carl A.
Stoney, William E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 18, 1954."Includes bibliographical references (p. 11).Mode of access: Internet

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.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)...

Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 /

Bare, E. Ann.
Haddad, Raymond C.
Reubush, David E.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 26).Mode of access: Inte...

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)....

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...

Comparisons of two-dimensional shock-expansion theory with experimental aerodynamic data for delta-planform wings at high supersonic speeds /

Jernell, Lloyd S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds /

Erickson, Gary E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 20-21).Mode of access: I...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

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 ...

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

McMillin, S. Naomi (Susan Naomi)
Murman, Earll M., 1942-
Thomas, James L. (James Lee), 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 98-99.Mode of access: Internet

Visualization of leading edge vortices on a series of flat plate delta wings /

Payne, Francis M.
Nelson, Robert C., 1942-
Ng, T. Terry.
Ames Research Center.
University of Notre Dame. Dept. of Aerospace and Mechanical Engineering.

January 1991

Prepared at the Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, for Ames Re...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds /

Sandahl, Carl A.
Stoney, William E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 18, 1954."Includes bibliographical references (p. 11).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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