Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"March 1965."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 /

Reubush, David E.
Runckel, Jack F.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 20-21.Mode of access: Internet

Effects of fineness and closure ratios on boattail drag of circular-arc afterbody models with jet exhaust at Mach numbers up to 1.3 /

Reubush, David E.
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 19-20.Mode of access: Inte...

Numerical calculation of transonic boattail flow /

Chow, Wen L.
Anderson, Bernhard H.
Bober, Lawrence J.
Lewis Research Center.

January 1975

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

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag /

Bromm, August F.
Goodwin, Julia M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"December 1, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets /

Whitcomb, Richard T.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

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

Calculation of the pressure distribution on axisymmetric boattails including effects of viscous interactions and exhaust jets in subsonic flow /

Rom, Josef, 1932-
Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal aerodynamic performance of a series of power-law and minimum-wave-drag bodies at Mach 6 and several Reynolds numbers /

Ashby, George C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"March 1965."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 /

Reubush, David E.
Runckel, Jack F.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 20-21.Mode of access: Internet

Effects of fineness and closure ratios on boattail drag of circular-arc afterbody models with jet exhaust at Mach numbers up to 1.3 /

Reubush, David E.
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 19-20.Mode of access: Inte...

Numerical calculation of transonic boattail flow /

Chow, Wen L.
Anderson, Bernhard H.
Bober, Lawrence J.
Lewis Research Center.

January 1975

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

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag /

Bromm, August F.
Goodwin, Julia M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"December 1, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds /

Bangert, Linda S.
Reubush, David E.
Leavitt, Laurence D.
Langley Research Center.

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 13).M...

A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets /

Whitcomb, Richard T.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

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

Calculation of the pressure distribution on axisymmetric boattails including effects of viscous interactions and exhaust jets in subsonic flow /

Rom, Josef, 1932-
Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal aerodynamic performance of a series of power-law and minimum-wave-drag bodies at Mach 6 and several Reynolds numbers /

Ashby, George C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"March 1965."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Abstract

Extracted data

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Abstract

Extracted data

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