The Two-dimensional Effects of Slipstream Shear on Airfoil Characteristics

The Two-dimensional Effects of Slipstream Shear on Airfoil Characteristics PDF Author: Robert J. Vidal
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 118

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The Two-dimensional Effects of Slipstream Shear on Airfoil Characteristics

The Two-dimensional Effects of Slipstream Shear on Airfoil Characteristics PDF Author: Robert J. Vidal
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 118

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The Effects of Axisymmetric Shear on Airfoil Characteristics

The Effects of Axisymmetric Shear on Airfoil Characteristics PDF Author: Robert J. Vidal
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 62

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1116

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Army Research Task Summary

Army Research Task Summary PDF Author: United States. Army Research Office
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 578

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Army Research Task Summary

Army Research Task Summary PDF Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 570

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Army Research Office, Fiscal Year 1961, Army Research Task Summary

Army Research Office, Fiscal Year 1961, Army Research Task Summary PDF Author: United States Department of the Army
Publisher:
ISBN:
Category :
Languages : en
Pages : 560

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Army Research Task Summary: Engineering sciences and earth sciences

Army Research Task Summary: Engineering sciences and earth sciences PDF Author: United States. Army Research Office
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 560

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NASA Contractor Report

NASA Contractor Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 320

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Theoretical and Experimental Studies of Airfoil Characteristics in Nonuniform Sheared Flow

Theoretical and Experimental Studies of Airfoil Characteristics in Nonuniform Sheared Flow PDF Author: William Gordon Brady
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 110

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Work is reported on a continuation of the experimental study of the two-dimensional wing in a three-dimensional sheared flow and also treats the theory of two-dimensional nonuniform sheared flows in an attempt to determine the mechanism responsible for the marked changes in airfoil stall characteristics which were demonstrated experimentally in Reference 3. It was felt desirable to complete the three-dimensional experimental program before resuming experimental work with two-dimensional nonuniform sheared flows. The experimental wing data obtained are presented and compared, where possible, with relevant two-dimensional data and with theory.

Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large-scale Six-propeller VTOL Model at Static Thrust

Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large-scale Six-propeller VTOL Model at Static Thrust PDF Author: Matthew M. Winston
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 76

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