Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail /

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron /

Moseley, William C., Jr.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 /

Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 121. ...

Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4 /

Schult, Eugene D.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 111. ...

Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45©� sweptback-wing--body combination /

Johnson, Harold S.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations /

Polhamus, Edward C.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 115. ...

Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section /

Johnson, Harold S.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

An experimental and theoretical investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic characteristics in sideslip of an unswept, untapered tail assembly /

Wiley, Harleth G.
Riley, Donald R.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45©� sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F., Jr.
Runckel, Jack F.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2©� delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"March 6, 1958."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

The twisting effect at transonic speeds of spoiler ailerons on a 45©� sweptback, aspect-ratio-4, tapered wing /

Hammond, Alexander D.
Graven, Jean C., Jr.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Comparison of full-scale lift and drag characteristics of the x-15 airplane with wind-tunnel results and theory /

Hopkins, Edward J.
Saltzman, Edwin J.
Fetterman, David E.
Flight Research Center (U.S.)
Langley Research Center.
Ames Research Center.

January 1962

"Classification changed to unclassified by authority of NASA CCN number 14, dated April 21, 1965."Ma...

Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 /

Gillis, Clarence L.
Vitale, A. James.
Langley Research Center.

January 1959

"NASA TN D-7.""Langley Research Center, Langley Field Va.""March 1960."Cover title.Includes bibliogr...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron /

Moseley, William C., Jr.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 /

Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 121. ...

Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4 /

Schult, Eugene D.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 111. ...

Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45©� sweptback-wing--body combination /

Johnson, Harold S.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations /

Polhamus, Edward C.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 115. ...

Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section /

Johnson, Harold S.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

An experimental and theoretical investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic characteristics in sideslip of an unswept, untapered tail assembly /

Wiley, Harleth G.
Riley, Donald R.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45©� sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F., Jr.
Runckel, Jack F.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2©� delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"March 6, 1958."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Hammond, Alexander D.
Graven, Jean C., Jr.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Comparison of full-scale lift and drag characteristics of the x-15 airplane with wind-tunnel results and theory /

Hopkins, Edward J.
Saltzman, Edwin J.
Fetterman, David E.
Flight Research Center (U.S.)
Langley Research Center.
Ames Research Center.

January 1962

"Classification changed to unclassified by authority of NASA CCN number 14, dated April 21, 1965."Ma...

Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 /

Gillis, Clarence L.
Vitale, A. James.
Langley Research Center.

January 1959

"NASA TN D-7.""Langley Research Center, Langley Field Va.""March 1960."Cover title.Includes bibliogr...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron /

Moseley, William C., Jr.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail /

Abstract

Extracted data

Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail /

Abstract

Extracted data

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