Author: Robert W. Dunning Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 692
Book Description
The data showed that transition always occurred along a front parallel to the wing leading edge, and that increasing the leading-edge sweep angle or increasing the angle of attack between the undisturbed stream and model surface caused the transition line to move closer to the wing leading edge and, in general, decreased the transition Reynolds number.
Author: United States. Superintendent of Documents Publisher: ISBN: Category : Government publications Languages : en Pages : 1434
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
Author: Robert W. Dunning
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Author: Battelle Memorial Institute
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Author: United States. Superintendent of Documents
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