Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft PDF Download

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Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft

Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft PDF Author: E. Richard White
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 28

Book Description


Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft

Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft PDF Author: E. Richard White
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 28

Book Description


Wind-Tunnel Investigation of Effects of Wing-Leading-Edge Modifications on the High Angle-Of-Attack Characteristics of a T-Tail Low-Wing General-Aviation Aircraft

Wind-Tunnel Investigation of Effects of Wing-Leading-Edge Modifications on the High Angle-Of-Attack Characteristics of a T-Tail Low-Wing General-Aviation Aircraft PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723419775
Category :
Languages : en
Pages : 26

Book Description
Exploratory tests have been conducted in the NASA-Langley Research Center's 12-Foot Low-Speed wind Tunnel to evaluate the application of wing-leading-edge devices on the stall-departure and spin resistance characteristics of a 1/6-scale model of a T-tail general-aviation aircraft. The model was force tested with an internal strain-gauge balance to obtain aerodynamic data on the complete configuration and with a separate wing balance to obtain aerodynamic data on the outer portion of the wing. The addition of the outboard leading-edge droop eliminated the abrupt stall of the windtip and maintained or increased the resultant-force coefficient up to about alpha = 32 degrees. This change in slope of the resultant-force coefficient curve with angle of attack has been shown to be important for eliminating autorotation and for providing spin resistance. White, E. R. Unspecified Center NASA-CR-3636, NAS 1.26:3636 NAS1-16000

Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft

Wind-tunnel Investigation of Effects of Wing-leading-edge Modifications on the High Angle-of-attack Characteristics of a T-tail Low-wing General-aviation Aircraft PDF Author: E. Richard White
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 28

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
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Languages : en
Pages : 420

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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ISBN:
Category : Government publications
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Category : Government publications
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Catalogue of Publications Issued by the Government of the United States PDF Author: United States. Superintendent of Documents
Publisher:
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Category : Government publications
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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

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Category : Aeronautics
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