Supersonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration

Supersonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 80

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Supersonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration

Supersonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 80

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Transonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration

Transonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 80

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Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air

Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air PDF Author: William I. Scallion
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

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A 0.0196-scale model of the HL-20 lifting body, one of several configurations proposed for future crewed spacecraft, was tested in the Langley 31-Inch Mach 10 Tunnel. The purpose of the tests was to determine the effectiveness of fin-mounted elevons, a lower surface flush-mounted body flap, and a flush-mounted yaw controller at hypersonic speeds. The nominal angle-of-attack range, representative of hypersonic entry, was 20 to 41 degrees, the sideslip angles were 0, 2, and -2 degrees, and the test Reynolds number was 1.06 x 10[factor 6] based on model reference length. The aerodynamic, longitudinal, and lateral control effectiveness along with surface oil flow visualizations are presented and discussed. The configuration was longitudinally and laterally stable at the nominal center of gravity. The primary longitudinal control, the fin-mounted elevons, could not trim the model to the desired entry angle of attack of 30 degrees. The lower surface body flaps were effective for roll control and the associated adverse yawing moment was eliminated by skewing the body flap hinge lines. A yaw controller, flush-mounted on the lower surface, was also effective, and the associated small rolling moment was favorable.

Subsonic Aerodynamic Characteristics of the HL-20 Lifting-body Configuration

Subsonic Aerodynamic Characteristics of the HL-20 Lifting-body Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 248

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1316

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 856

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Langley Aerospace Test Highlights, 1990

Langley Aerospace Test Highlights, 1990 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 188

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Large Space Structures & Systems in the Space Station Era

Large Space Structures & Systems in the Space Station Era PDF Author:
Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 356

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