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

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).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

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

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 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...

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 /

Sevier, John R.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 12).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 in pitch and sideslip of a 1/15-scale model of the Scout vehicle at a mach number of 2.01 /

Robinson, Ross B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers; S...

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 of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

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

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 /

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

January 1952

"July 28, 1952."Includes bibliographical references (p. 7-8).Mode of access: Internet

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

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

Cover title." April 1962."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles, Stabilit...

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

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).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

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

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 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...

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 /

Sevier, John R.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 12).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 in pitch and sideslip of a 1/15-scale model of the Scout vehicle at a mach number of 2.01 /

Robinson, Ross B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers; S...

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 of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

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

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 /

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

January 1952

"July 28, 1952."Includes bibliographical references (p. 7-8).Mode of access: Internet

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

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

Cover title." April 1962."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles, Stabilit...

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

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).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

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

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

Abstract

Extracted data

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

Abstract

Extracted data

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