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Measurements Of The Static Pressure Distributions And Shock Shape On An Oblate Spheroid At Mach Numbers Of 3 And 6
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Book Synopsis Measurements of the Static Pressure Distributions and Shock Shape on an Oblate Spheroid at Mach Numbers of 3 and 6 by :
Download or read book Measurements of the Static Pressure Distributions and Shock Shape on an Oblate Spheroid at Mach Numbers of 3 and 6 written by and published by . This book was released on 1966 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of experimental measurements of the static pressure distribution and bow shock shape on an oblate spheroid are presented. This experiment was conducted at nominal Mach numbers of 3 and 6 and a free stream Reynolds number range of 2,300,000 to 5,800,000 per foot. Comparisons are made with the calculated values of several different laboratories.
Book Synopsis Measurements of the Static Pressure Distributions and Shock Shape on an Oblate Spheroid at Mach Numbers of 3 and 6 by : Lionel Pasiuk
Download or read book Measurements of the Static Pressure Distributions and Shock Shape on an Oblate Spheroid at Mach Numbers of 3 and 6 written by Lionel Pasiuk and published by . This book was released on 1966 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of experimental measurements of the static pressure distribution and bow shock shape on an oblate spheroid are presented. This experiment was conducted at nominal Mach numbers of 3 and 6 and a free stream Reynolds number range of 2,300,000 to 5,800,000 per foot. Comparisons are made with the calculated values of several different laboratories.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1967 with total page 1058 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 760 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government-wide Index to Federal Research & Development Reports by :
Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1966 with total page 1466 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis U.S. Government Research & Development Reports by :
Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1966-11 with total page 1014 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mathematical Methods in Fluid Mechanics by :
Download or read book Mathematical Methods in Fluid Mechanics written by and published by . This book was released on 1980 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Journal of the Royal Aeronautical Society by :
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1966 with total page 1304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722054021 Total Pages :28 pages Book Rating :4.0/5 (54 download)
Book Synopsis Aerodynamics of a Sphere and an Oblate Spheroid for Mach Numbers from 0. 6 to 10. 5 Including Some Effects of Test Conditions by : National Aeronautics and Space Administration (NASA)
Download or read book Aerodynamics of a Sphere and an Oblate Spheroid for Mach Numbers from 0. 6 to 10. 5 Including Some Effects of Test Conditions written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-20 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests were made for spheres of various sizes over a range of Mach numbers and Reynolds numbers. The results indicated some conditions where the drag was affected by changes in the afterbody pressure due to a shock reflection from the tunnel wall. This effect disappeared when the Mach number was increased for a given sphere size or when the sphere size was decreased for a given Mach number. Drag measurements and Schlieren photographs are presented that show the possibility of obtaining inaccurate data when tests are made with a sphere too large for the test section size and Mach number. Tests were also made of an oblate spheroid. The results indicated a region at high Mach numbers where inherent positive static stability might occur with the oblate-face forward. The drag results are compared with those for a sphere as well as those for various other shapes. The drag results for the oblate spheroid and the sphere are also compared with some calculated results. Spearman, M. Leroy and Braswell, Dorothy O. Langley Research Center RTOP 505-69-20-01...
Book Synopsis Flow-field Measurements Downstream of Two Protuberances on a Flat Plate Submerged in a Turbulent Boundary Layer at Mach 2.49 and 4.44 by : Lana M. Couch
Download or read book Flow-field Measurements Downstream of Two Protuberances on a Flat Plate Submerged in a Turbulent Boundary Layer at Mach 2.49 and 4.44 written by Lana M. Couch and published by . This book was released on 1969 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of a Sphere and an Oblate Spheroid for Mach Numbers from 0. 6 to 10. 5 Including Some Effects of Test Conditions by : National Aeronautics and Space Administration NASA
Download or read book Aerodynamics of a Sphere and an Oblate Spheroid for Mach Numbers from 0. 6 to 10. 5 Including Some Effects of Test Conditions written by National Aeronautics and Space Administration NASA and published by . This book was released on 2018-10-23 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests were made for spheres of various sizes over a range of Mach numbers and Reynolds numbers. The results indicated some conditions where the drag was affected by changes in the afterbody pressure due to a shock reflection from the tunnel wall. This effect disappeared when the Mach number was increased for a given sphere size or when the sphere size was decreased for a given Mach number. Drag measurements and Schlieren photographs are presented that show the possibility of obtaining inaccurate data when tests are made with a sphere too large for the test section size and Mach number. Tests were also made of an oblate spheroid. The results indicated a region at high Mach numbers where inherent positive static stability might occur with the oblate-face forward. The drag results are compared with those for a sphere as well as those for various other shapes. The drag results for the oblate spheroid and the sphere are also compared with some calculated results. Spearman, M. Leroy and Braswell, Dorothy O. Langley Research Center RTOP 505-69-20-01...
Book Synopsis U. S. Government Research and Development Reports by :
Download or read book U. S. Government Research and Development Reports written by and published by . This book was released on 1966-10 with total page 1452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1994 with total page 1372 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Pressure Distribution and Shock-wave Shape on Power-law Bodies at a Mach Number of 6.85 by : D. H. Peckham
Download or read book Measurements of Pressure Distribution and Shock-wave Shape on Power-law Bodies at a Mach Number of 6.85 written by D. H. Peckham and published by . This book was released on 1967 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of a Sphere and an Oblate Spheroid for Mach Numbers from 0.6 to 10.5 Including Some Effects of Test Conditions by : M. Leroy Spearman
Download or read book Aerodynamics of a Sphere and an Oblate Spheroid for Mach Numbers from 0.6 to 10.5 Including Some Effects of Test Conditions written by M. Leroy Spearman and published by . This book was released on 1993 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1966-10 with total page 1020 pages. Available in PDF, EPUB and Kindle. Book excerpt:
