Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing

Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing PDF Author: Thomas A. Byrdsong
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ISBN:
Category :
Languages : en
Pages : 100

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Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing

Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing PDF Author: Thomas A. Byrdsong
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

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Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing. Supplement

Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing. Supplement PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 272

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Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Superficial Wing

Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Superficial Wing PDF Author: Thomas A. Byrdsong
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 100

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Steady Pressure Measurements on an Aeroelastic Research Wing (ARW-2)

Steady Pressure Measurements on an Aeroelastic Research Wing (ARW-2) PDF Author: Maynard C. Sandford
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 582

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 272

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 496

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Close-Range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing

Close-Range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing PDF Author: National Aeronautics and Space Adm Nasa
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ISBN: 9781730933172
Category :
Languages : en
Pages : 94

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Close range photogrammetric measurements were made for the lower wing surface of a full span aspect ratio 10.3 aeroelastic supercritical research wing. The measurements were made during wind tunnel tests for quasi-steady pressure distributions on the wing. The tests were conducted in the NASA Langley Transonic Dynamics Tunnel at Mach numbers up to 0.90 and dynamic pressures up to 300 pounds per square foot. Deflection data were obtained for 57 locations on the wing lower surface using dual non-metric cameras. Representative data are presented as graphical overview to show variations and trends of spar deflection with test variables. Comparative data are presented for photogrammetric and cathetometric results of measurements for the wing tip deflections. A tabulation of the basic measurements is presented in a supplement to this report. Byrdsong, Thomas A. and Adams, Richard R. and Sandford, Maynard C. Langley Research Center...

NASA SP.

NASA SP. PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 654

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 648

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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 274)

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 274) PDF Author:
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ISBN:
Category :
Languages : en
Pages : 648

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