Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Low-speed Wind-tunnel Tests of the Effects of Various Leading-edge Modifications on the Sectional Characteristics of a Thin Wing (6% Thick, R.A.E. 101 Section).
Author: Low speed wind tunnel tests of the effect of various leading edge modifications on the sectional characteristics of a thin wing
Author: S. F. J. ButlerLow-speed Wind-tunnel Tests of the Effects of Various Leading-edge Modifications on the Sectional Characteristics of a Thin Wing
Author: Aeronautical Research CouncilPublisher:
ISBN:
Category :
Languages : en
Pages : 26
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
Author: E. Richard WhitePublisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 28
Book Description
Applied Mechanics Reviews
Author: Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model
Author: Byron M. JaquetPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
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
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
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
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.
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1366
Book Description