Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section /

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

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

Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft /

Allison, Dennis O.
Waggoner, E. G.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 11.Mode of access: Internet

Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil /

Beasley, William D.
McGhee, William D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

On the formulation of the aerodynamic characteristics in aircraft dynamics /

Tobak, Murray.
Schiff, Lewis B.
Ames Research Center.

January 1976

Prepared at Ames Research Center."Corrected copy."Cover title.Includes bibliographical references (p...

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil /

Yu, James C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

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

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

The Influence of sweep on the aerodynamic loading of an oscillating NACA 0012 airfoil /

St. Hilaire, A. O.
United States. National Aeronautics and Space Administration.

January 1979

"Contract NAS1-14873.""May 1979"--Cover.Includes bibliographical references.v. 1. Technical report.M...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Apr. 1979."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

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

Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft /

Allison, Dennis O.
Waggoner, E. G.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 11.Mode of access: Internet

Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil /

Beasley, William D.
McGhee, William D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

On the formulation of the aerodynamic characteristics in aircraft dynamics /

Tobak, Murray.
Schiff, Lewis B.
Ames Research Center.

January 1976

Prepared at Ames Research Center."Corrected copy."Cover title.Includes bibliographical references (p...

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil /

Yu, James C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

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

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

The Influence of sweep on the aerodynamic loading of an oscillating NACA 0012 airfoil /

St. Hilaire, A. O.
United States. National Aeronautics and Space Administration.

January 1979

"Contract NAS1-14873.""May 1979"--Cover.Includes bibliographical references.v. 1. Technical report.M...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Apr. 1979."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

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

Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft /

Allison, Dennis O.
Waggoner, E. G.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 11.Mode of access: Internet

Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section /

Abstract

Extracted data

Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section /

Abstract

Extracted data

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