Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

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 ...

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7

Kussoy, Marvin.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Pressure measurements on two 60° swept delta wings with blunt leading edges and dihedral angles of 0° and 45° at a Mach number of 4.95. Calvin Stainback.

Stainback, P. Calvin.
United States. National Aeronautics and Space Administration.

January 1962

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles; Fluid mechanics; Stresses a...

Tabulated data from a pressure-distribution investigation at mach number 2.01 of the wing of a canard airplane model /

Driver, Cornelius.
Jacocks, James L.
Langley Research Center.

January 1959

"December 1959"--Cover.Caption title.Includes bibliographical references (p. 5).Mode of access: Inte...

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 /

Cooper, Morton.
Gunn, Charles R.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inte...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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)...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

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 ...

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7

Kussoy, Marvin.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Pressure measurements on two 60° swept delta wings with blunt leading edges and dihedral angles of 0° and 45° at a Mach number of 4.95. Calvin Stainback.

Stainback, P. Calvin.
United States. National Aeronautics and Space Administration.

January 1962

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles; Fluid mechanics; Stresses a...

Tabulated data from a pressure-distribution investigation at mach number 2.01 of the wing of a canard airplane model /

Driver, Cornelius.
Jacocks, James L.
Langley Research Center.

January 1959

"December 1959"--Cover.Caption title.Includes bibliographical references (p. 5).Mode of access: Inte...

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 /

Cooper, Morton.
Gunn, Charles R.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inte...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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)...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

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 ...

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Abstract

Extracted data

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Abstract

Extracted data

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