Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

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:...

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...

Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration /

Murri, Daniel G.
Grafton, Sue B.
Nguyen, Luat T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

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

Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration /

Grafton, Sue B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration /

Maki, Ralph L.
Giulianetti, Demo J.
Ames Research Center.

January 1959

"NASA TN D-16.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Includes bibli...

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Satran, Dale R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 /

Mann, Michael J.
Campbell, Richard L. (Richard Lawson), 1952-
Mercer, Charles E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes bibliographical references.Mode of access:...

Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ /

Mann, Michael J.
Fox, Charles H.
Huffman, Jarrett K.
Langley Research Center.

January 1987

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

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

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:...

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...

Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration /

Murri, Daniel G.
Grafton, Sue B.
Nguyen, Luat T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

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

Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration /

Grafton, Sue B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration /

Maki, Ralph L.
Giulianetti, Demo J.
Ames Research Center.

January 1959

"NASA TN D-16.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Includes bibli...

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Satran, Dale R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 /

Mann, Michael J.
Campbell, Richard L. (Richard Lawson), 1952-
Mercer, Charles E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes bibliographical references.Mode of access:...

Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ /

Mann, Michael J.
Fox, Charles H.
Huffman, Jarrett K.
Langley Research Center.

January 1987

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

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

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:...

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...

Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration /

Murri, Daniel G.
Grafton, Sue B.
Nguyen, Luat T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Abstract

Extracted data

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Abstract

Extracted data

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