Some Recent Applications of the Suction Analogy to Vortex-lift Estimates

Some Recent Applications of the Suction Analogy to Vortex-lift Estimates PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Some Recent Applications of the Suction Analogy to Vortex-lift Estimates

Some Recent Applications of the Suction Analogy to Vortex-lift Estimates PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 600

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Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack

Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack PDF Author: James M. Luckring
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 992

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Application of the Leading-edge-suction Analogy of Vortex Lift to the Drag Due to Lift of Sharp-edge Delta Wings

Application of the Leading-edge-suction Analogy of Vortex Lift to the Drag Due to Lift of Sharp-edge Delta Wings PDF Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 18

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NASA Conference Publication

NASA Conference Publication PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 432

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 166

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Aerodynamic Analyses Requiring Advanced Computers

Aerodynamic Analyses Requiring Advanced Computers PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 788

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 888

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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)

Transonic Pressure Measurements and Comparison of Theory to Experiment for an Arrow-wing Configuration

Transonic Pressure Measurements and Comparison of Theory to Experiment for an Arrow-wing Configuration PDF Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 500

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A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings as well as a variety of leading- and trailing-edge control surface deflections, was conducted at Mach numbers from 0.4 to 1.1 to provide an experimental pressure data base for comparison with theoretical methods. Theory-to-experiment comparisons of detailed pressure distributions were made using current state-of-the-art attached and separated flow methods. The purpose of these comparisons was to delineate conditions under which these theories are valid for both flat and twisted wings and to explore the use of empirical methods to correct the theoretical methods where theory is deficient. The results are summarized.