Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers /

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio /

Johnston, Patrick J.
Witcofski, Robert D.
Langley Research Center.

Prepared at Langley Research Center."February 1968"--Cover.Includes bibliographical references (p. 1...

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

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

Levy, Lionel L.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

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

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

West, F. E.
United States. National Aeronautics and Space Administration.

Cover title." November 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and l...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Aerodynamic tests and analysis of a turbojet-boosted launch vehicleconcept (spacejet) over a Mach number range of 1.50 to 2.86 /

Riebe, Gregory D.
Morris, Odell A.
Small, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."July 1981"--Cover."Langley Research Center."Includes bibliographical references...

Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 /

Stone, Howard W.
Powell, Richard W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method /

Tuovila, W. J. (Weimer J.)
Hess, R. W. (Robert W.)
Langley Research Center.

January 1960

"NASA TN D-116.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includ...

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

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

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mecha...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio /

Johnston, Patrick J.
Witcofski, Robert D.
Langley Research Center.

Prepared at Langley Research Center."February 1968"--Cover.Includes bibliographical references (p. 1...

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

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

Levy, Lionel L.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

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

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

West, F. E.
United States. National Aeronautics and Space Administration.

Cover title." November 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and l...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Aerodynamic tests and analysis of a turbojet-boosted launch vehicleconcept (spacejet) over a Mach number range of 1.50 to 2.86 /

Riebe, Gregory D.
Morris, Odell A.
Small, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."July 1981"--Cover."Langley Research Center."Includes bibliographical references...

Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 /

Stone, Howard W.
Powell, Richard W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method /

Tuovila, W. J. (Weimer J.)
Hess, R. W. (Robert W.)
Langley Research Center.

January 1960

"NASA TN D-116.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includ...

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

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

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mecha...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers /

Abstract

Extracted data

Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers /

Abstract

Extracted data

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