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Effect Of Leading Edge Thickness On The Flow Over A Flat Plate At A Mach Number Of 57
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Book Synopsis Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 by : Marcus O. Creager
Download or read book Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 written by Marcus O. Creager and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 by : Marcus O. Creager
Download or read book Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 written by Marcus O. Creager and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Leading Edge Effect on the Flow Over a Flat Plate at M by : James Courtland Townsend
Download or read book The Leading Edge Effect on the Flow Over a Flat Plate at M written by James Courtland Townsend and published by . This book was released on 1966 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the leading edge effects on the flow over a flat plate was made at a Mach number of 10. The Reynolds number based on free stream conditions and leading edge thickness varied from 115, where viscous effects predominated, to 14,550, where inviscid effects predominated. Shock wave shape and pressure and heat transfer distributions over the plate were obtained. In general, good agreement existed between the measurements and the various theories. The use of appropriate parameters allowed the results to be compared with those of a similar study using helium as the test fluid. Good correlation was found between the measurements made in air and in helium. (Author).
Book Synopsis The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 by : Howard W. Stone
Download or read book The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 written by Howard W. Stone and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1966 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7 by : Thorval Tendeland
Download or read book The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7 written by Thorval Tendeland and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis WADC Technical Report by : United States. Wright Air Development Division
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1957 with total page 1502 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Simple Solutions to the Problem of Predicting Boundary-layer Self-induced Pressures by : Michael H. Bertram
Download or read book Some Simple Solutions to the Problem of Predicting Boundary-layer Self-induced Pressures written by Michael H. Bertram and published by . This book was released on 1961 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate by : Don W. Jillie
Download or read book Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate written by Don W. Jillie and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 860 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Vortex Flows at Supersonic Speeds by : Richard M. Wood
Download or read book Vortex Flows at Supersonic Speeds written by Richard M. Wood and published by . This book was released on 2003 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1961 with total page 1274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1961 with total page 1284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wall Cooling and Leading-edge Blunting on Ramp-induced, Laminar Flow Separations at Mach Numbers from 3 Through 6 by : J. Don Gray
Download or read book Effects of Wall Cooling and Leading-edge Blunting on Ramp-induced, Laminar Flow Separations at Mach Numbers from 3 Through 6 written by J. Don Gray and published by . This book was released on 1972 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.
Book Synopsis Index to NASA Technical Publications by : United States. National Aeronautics and Space Administration
Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1968 with total page 1366 pages. Available in PDF, EPUB and Kindle. Book excerpt:
