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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)
Download or read book Pressure Distribution on a Flat-bottom Canted Nose Half-cone Reentry Configuration at a Mach Number of 6.0 written by and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 908 pages
Book Rating : 4.E/5 ( download)
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 908 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : G. B. Marson
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ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (11 download)
Download or read book An Experimental Investigation of the Pressure Distributions on Five Bodies of Revolution at Mach Numbers of 2.45 and 3.19 written by G. B. Marson and published by . This book was released on 1954 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (317 download)
Download or read book Pressure Distribution on a Blunt-leading-edge Modified-delta-planform Reentry Configuration at a Mach Number of 6.0 written by and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James N. Mueller
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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)
Download or read book An Investigation of Induced-pressure Phenomena on Axially Symmetric, Flow-alined, Cylindrical Models Equipped with Different Nose Shapes at Free-stream Mach Numbers from 15.6 to 21 in Helium written by James N. Mueller and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)
Download or read book Pressure Distribution at a Mach Number of 24.5 on a Symmetrical Blunt-faced Reentry Body at Angles of Attack from 0 Deg to 40 Deg in Helium Including an Investigation of Afterbody Sting Effects written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : G. B. Marson
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ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (165 download)
Download or read book An Experimental Investigation of the Pressure Distribution on Five Bodies of Revolution at Mach Numbers of 2.45 and 3.19 written by G. B. Marson and published by . This book was released on 1954 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 1368 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1983 with total page 1368 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 202 pages
Book Rating : 4.:/5 (227 download)
Download or read book STATIC PRESSURE DISTRIBUTIONS ON VARIOUS BODIES OF REVOLUTION AT MACH NUMBERS FROM 0.60 TO 1.60 written by and published by . This book was released on 1968 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Propulsion Wind Tunnel, Transonic (16T) to determine the static pressure distributions on various bodies of revolution. The nose shapes tested were 20-, 40-, and 60-deg (total-angle) cones, an ellipse, and an ogive. The data were obtained for various angles of pitch and yaw at Mach numbers from 0.60 to 1.60. Primarily these data will be used for the test section calibration of a new transonic wind tunnel with a 4- ft-square test section; consequently, the models were designed for 1-percent blockage in the 4-ft wind tunnel, making them 0.0625-percent blockage in Tunnel 16T. Despite their relatively small size in 16T, some wall effects were experienced between Mach numbers 0.95 and 1.05. Both above and below this Mach number range the data were found to be relatively free of wall effects. In the range from M = 0.95 to 1.05 attempts were made to reduce the wall effects by varying wall angle and test section pressure.
Author : Raymond H. Eaves
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ISBN 13 :
Total Pages : 59 pages
Book Rating : 4.:/5 (782 download)
Download or read book An Empirical Correlation of Pressure on Blunt-nosed Cylindrical Afterbodies at Hypersonic Mach Numbers written by Raymond H. Eaves and published by . This book was released on 1968 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 344 pages
Book Rating : 4.F/5 ( download)
Download or read book Hypersonic Aerothermodynamics written by and published by . This book was released on 1984 with total page 344 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 STATIC PRESSURE DISTRIBUTIONS ON VARIOUS BODIES OF REVOLUTION AT MACH NUMBERS FROM 0.60 TO 1.60 written by and published by . This book was released on 1968 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Propulsion Wind Tunnel, Transonic (16T) to determine the static pressure distributions on various bodies of revolution. The nose shapes tested were 20-, 40-, and 60-deg (total-angle) cones, an ellipse, and an ogive. The data were obtained for various angles of pitch and yaw at Mach numbers from 0.60 to 1.60. Primarily these data will be used for the test section calibration of a new transonic wind tunnel with a 4- ft-square test section; consequently, the models were designed for 1-percent blockage in the 4-ft wind tunnel, making them 0.0625-percent blockage in Tunnel 16T. Despite their relatively small size in 16T, some wall effects were experienced between Mach numbers 0.95 and 1.05. Both above and below this Mach number range the data were found to be relatively free of wall effects. In the range from M = 0.95 to 1.05 attempts were made to reduce the wall effects by varying wall angle and test section pressure.
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ISBN 13 :
Total Pages : 924 pages
Book Rating : 4.3/5 (243 download)
Download or read book NASA SP. written by and published by . This book was released on 1962 with total page 924 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael E. Tauber
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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Review of High-speed, Convective, Heat-transfer Computation Methods written by Michael E. Tauber and published by . This book was released on 1989 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 686 pages
Book Rating : 4.:/5 (26 download)
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1967 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Johns Hopkins University. Applied Physics Laboratory
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ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.3/5 (91 download)
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1952 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Aeronautics and Space Administration
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ISBN 13 :
Total Pages : 340 pages
Book Rating : 4.3/5 (91 download)
Download or read book Space Scientists and Engineers: Selected Biographical and Bibliographical Listing written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
