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Author :
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (317 download)
Download or read book Investigation of Three Mach 7 External Compression Axisymmetric Inlets from Mach 1.9 to 6.8 written by and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Owen H. Davis
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79 written by Owen H. Davis and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John L. Allen
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)
Download or read book Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8 written by John L. Allen and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
![Download Performance of Mach No. 3.0 Design Axisymmetric Double-cone External-compression Inlet in Mach Number Range 2.07 to 1.48 [with List of References] PDF Online Free](https://books.google.com/books/content/images/frontcover/uli0wgEACAAJ?fife=w200-h370)
Author : John L. Allen
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (18 download)
Download or read book Performance of Mach No. 3.0 Design Axisymmetric Double-cone External-compression Inlet in Mach Number Range 2.07 to 1.48 [with List of References] written by John L. Allen and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (317 download)
Download or read book Performance of a Mach 3.0 External-internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5 written by and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)
Download or read book PERFORMANCE SUMMARY AND ANALYSIS OF A MACH 3.0 DESIGN AXISYMMETRIC ALL-EXTERNAL-COMPRESSION DOUBLE-CONE INLET FROM MACH NUMBER 3.0 TO 0.8 written by and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John L. Allen
Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (11 download)
Download or read book Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All External Compression Double Cone Inlet Form Mach Number 3.0 - 0.8 written by John L. Allen and published by . This book was released on 1960 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John L. Allen
Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (761 download)
Download or read book Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8 written by John L. Allen and published by . This book was released on 1960 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John L. Allen
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (471 download)
Download or read book Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in Mach Number Range 2.07 to 1.48 written by John L. Allen and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)
Download or read book Investigation of the Performance and Control of a Mach 3.0, Two-dimensional, External-internal-compression Inlet written by and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 854 pages
Book Rating : 4.:/5 (319 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1974 with total page 854 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 952 pages
Book Rating : 4.E/5 ( download)
Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1968 with total page 952 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Warren R. Hingst
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ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (11 download)
Download or read book Experimental Investigation of Boundary Layers in an Axisymmetric Mach 2.5, Mixed Compression Inlet written by Warren R. Hingst and published by . This book was released on 1973 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)
Download or read book Investigation of the Flow Over an Axisymmetric Compression Surface at High Mach Numbers written by and published by . This book was released on 1961 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Axisymmetric compression surfaces designed for Mach number 7 were fired as projectiles in the NOL pressurized ballistics range no. 3. Range pressures varied from approximately 100 to 300 mm of mercury with a few firings at 1 atmosphere. Range temperature was the ambient or room temperature. Mach numbers from 4.5 to 7.4 were recorded. Results are presented in the form of spark photographs from which data on flow fields and boundary-layer conditions were obtained. The data are analyzed and compared with theory. Although the wall temperatures are too low for simulation of a flight case and the boundary layer appears laminar, the results are of general interest because they represent conditions with a thin boundary layer on a cold surface. A strong effect of wall temperature on separation is noted. (Author).
Author : Richard J. Re
Publisher :
ISBN 13 :
Total Pages : 150 pages
Book Rating : 4.F/5 ( download)
Download or read book An Investigation of Several NACA 1-series Axisymmetric Inlets at Mach Numbers from 0.4 to 1.29 written by Richard J. Re and published by . This book was released on 1974 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T. W. Tsukahira
Publisher :
ISBN 13 :
Total Pages : 904 pages
Book Rating : 4.3/5 (91 download)
Download or read book Supersonic Inlet Investigation written by T. W. Tsukahira and published by . This book was released on 1971 with total page 904 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reported herein are the results of an investigation whose primary objective was to develop design criteria and performance tradeoffs for supersonic inlets applicable to advanced tactical aircraft. The objective was accomplished by conducting analysis and wind tunnel tests. The baseline models included a two-dimensional external compression inlet, a two-dimensional mixed compression inlet, and a half-axisymmetric external compression inlet. Alternate configurations for the external compression baseline inlets in the AEDC PWT-4T and VKF-A wind tunnels, respectively. The inlets were tested both isolated and in a non-uniform flow field, the later representing partial simulation of a vehicle flow field. Inlet steady state performance was characterized in terms of pressure recovery, pressure distortion, and turbulence levels at a simulated compressor face and immediately downstream of the inlet throat. In addition, detailed analysis and correlation of data obtained with high response dynamic instrumentation were made.
Author : United States. Superintendent of Documents
Publisher :
ISBN 13 :
Total Pages : 1304 pages
Book Rating : 4.E/5 ( download)
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 1963 with total page 1304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
