Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

Foster, Gerald V.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 /

Hopkins, Edward J.
Carmichael, Ralph L.
Hicks, Raymond M.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"October 1967."Includes bibliographical references (p.21).Mode of access: Internet

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical reference (p. 9).Mode of access: Internet

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

The aerodynamic characteristics of a body in the flow field near the tip of a circular-arc wing of rectangular plan form at a mach number of 2.01 /

Gapcynski, John P.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Aerodynamic characteristics of a 60° sweptback-wing airplane configuration having tail surfaces located outboard of the wingtips at mach numbers of 2.30, 2.97, 3.51, and 4.06 /

Sleeman, Jr., William C.
Fournier, Roger H.
Church, James D.
Langley Research Center.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75° /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

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

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

Foster, Gerald V.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 /

Hopkins, Edward J.
Carmichael, Ralph L.
Hicks, Raymond M.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"October 1967."Includes bibliographical references (p.21).Mode of access: Internet

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical reference (p. 9).Mode of access: Internet

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

The aerodynamic characteristics of a body in the flow field near the tip of a circular-arc wing of rectangular plan form at a mach number of 2.01 /

Gapcynski, John P.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Aerodynamic characteristics of a 60° sweptback-wing airplane configuration having tail surfaces located outboard of the wingtips at mach numbers of 2.30, 2.97, 3.51, and 4.06 /

Sleeman, Jr., William C.
Fournier, Roger H.
Church, James D.
Langley Research Center.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75° /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

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

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

Foster, Gerald V.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Abstract

Extracted data

Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Abstract

Extracted data

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