Supersonic wings with significant leading-edge thrust at cruise /

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

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 ...

Supersonic cruise military aircraft research : an annotated bibliography /

Tuttle, Marie H.
Maddalon, Dal V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Includes index."April 1980"--Cover."Langley Research Center."Mode of access: Internet

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...

Study of supersonic wings employing the attainable leading-edge thrust concept /

Middleton, W. D. (Wilbur D.), 1931-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Boeing Commercial Airplane Company.
Langley Research Center.

January 1982

"Boeing Commercial Airplane Company.""November 1982"--Cover.Includes bibliographical references.Mode...

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

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)....

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)...

Historical background and design evolution of the transonic aircraft technology supercritical wing /

Ayers, Theodore G.
Hallissy, James B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Hugh L. Dryden Flight Research Center.

January 1981

STAR category 02."Langley Research Center.""August 1981"--Cover."Dryden Flight Research Center."Incl...

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /

Stallings, Robert L.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"July 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

Estimation of attainable leading-edge thrust for wings at subsonicaand supersonic speeds

Carlson, Harry W.
Barger, Raymond L.
Mack, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 /

Riebe, Gregory D.
Pittman, Jimmy L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover."Langley Research Center."Mode of access: Internet

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

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 ...

Supersonic cruise military aircraft research : an annotated bibliography /

Tuttle, Marie H.
Maddalon, Dal V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Includes index."April 1980"--Cover."Langley Research Center."Mode of access: Internet

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...

Study of supersonic wings employing the attainable leading-edge thrust concept /

Middleton, W. D. (Wilbur D.), 1931-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Boeing Commercial Airplane Company.
Langley Research Center.

January 1982

"Boeing Commercial Airplane Company.""November 1982"--Cover.Includes bibliographical references.Mode...

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

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)....

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)...

Historical background and design evolution of the transonic aircraft technology supercritical wing /

Ayers, Theodore G.
Hallissy, James B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Hugh L. Dryden Flight Research Center.

January 1981

STAR category 02."Langley Research Center.""August 1981"--Cover."Dryden Flight Research Center."Incl...

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /

Stallings, Robert L.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"July 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

Estimation of attainable leading-edge thrust for wings at subsonicaand supersonic speeds

Carlson, Harry W.
Barger, Raymond L.
Mack, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 /

Riebe, Gregory D.
Pittman, Jimmy L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover."Langley Research Center."Mode of access: Internet

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

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 ...

Supersonic wings with significant leading-edge thrust at cruise /

Abstract

Extracted data

Supersonic wings with significant leading-edge thrust at cruise /

Abstract

Extracted data

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