Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6

Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6 PDF Author: Edward Charles Polhamus
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Category : Aerodynamics
Languages : en
Pages : 48

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Book Description
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect ratio on the aerodynamic characteristics of parawings. To determine the effects of camber and twist, tests were made both with the conventional conical-type canopy, which provides camber and washout, and with a cylindrical-type canopy which provides essentially zero camber and twist. With regard to aspect ratio, tests were made of parawings having aspect ratios of 3 and 6; the range was thereby extended well beyond that of previous investigations. The degree to which airfoil and wing theory can be used to predict the aerodynamic characteristics of parawings was also investigated.

Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6

Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6 PDF Author: Edward Charles Polhamus
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

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Book Description
Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect ratio on the aerodynamic characteristics of parawings. To determine the effects of camber and twist, tests were made both with the conventional conical-type canopy, which provides camber and washout, and with a cylindrical-type canopy which provides essentially zero camber and twist. With regard to aspect ratio, tests were made of parawings having aspect ratios of 3 and 6; the range was thereby extended well beyond that of previous investigations. The degree to which airfoil and wing theory can be used to predict the aerodynamic characteristics of parawings was also investigated.

NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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Category : Aeronautics
Languages : en
Pages : 262

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
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Category : Mechanics, Applied
Languages : en
Pages : 1196

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Category : Aeronautics
Languages : en
Pages : 258

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The Journal of the Royal Aeronautical Society

The Journal of the Royal Aeronautical Society PDF Author: Royal Aeronautical Society
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Category : Aeronautics
Languages : en
Pages : 1168

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A Selected Listing of Nasa Scientific and Technical Reports for 1963

A Selected Listing of Nasa Scientific and Technical Reports for 1963 PDF Author:
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Category :
Languages : en
Pages : 254

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NASA SP.

NASA SP. PDF Author:
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Category : Aeronautics
Languages : en
Pages : 262

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Journal of the Royal Aeronautical Society PDF Author:
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Category : Aeronautics
Languages : en
Pages : 950

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
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Category :
Languages : en
Pages : 642

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
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Category : Aeronautics
Languages : en
Pages : 608

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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).