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Measurements Of Blast Induced Transient Pressures At The Base Of A Cone In Supersonic Flow
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Book Synopsis Measurements of Blast-induced Transient Pressures at the Base of a Cone in Supersonic Flow by : Frank P. Baltakis
Download or read book Measurements of Blast-induced Transient Pressures at the Base of a Cone in Supersonic Flow written by Frank P. Baltakis and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transient pressures, induced by a head-on blast wave, were measured at the base of a nine-degree half-angle cone in a supersonic stream using a wind-tunnel shocktube technique. Tests were conducted at free-stream Mach numbers of 3, 5 and 6.5 and at blast wave Mach numbers of 1.5 to 3, 2 to 5 and 4 to 8 at free-stream Mach numbers of 3, 5 and 6.5, respectively. Within the range of this experiment, shock-induced base pressure was found to increase approximately in proportion to the blast wave Mach number squared. When expressed in ratio to the free-stream static pressure, the induced base pressure was found to decrease, approximately, linearly with increasing free-stream Mach number. At the free-stream/blast wave Mach number conditions of 3/3, 5/5 and 6.5/8 the respective induced base pressure to initial free-stream static pressure ratios were 5, 8 and 18. (Author).
Book Synopsis Measurements of Blast-Induced Transient Pressures at the Base of a Cone in Supersonic Flow by : Frank P. Baltakis
Download or read book Measurements of Blast-Induced Transient Pressures at the Base of a Cone in Supersonic Flow written by Frank P. Baltakis and published by . This book was released on 1969 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transient pressures, induced by a head-on blast wave, were measured at the base of a nine-degree half-angle cone in a supersonic stream using a wind-tunnel shocktube technique. Tests were conducted at free-stream Mach numbers of 3, 5 and 6.5 and at blast wave Mach numbers of 1.5 to 3, 2 to 5 and 4 to 8 at free-stream Mach numbers of 3, 5 and 6.5, respectively. Within the range of this experiment, shock-induced base pressure was found to increase approximately in proportion to the blast wave Mach number squared. When expressed in ratio to the free-stream static pressure, the induced base pressure was found to decrease, approximately, linearly with increasing free-stream Mach number. At the free-stream/blast wave Mach number conditions of 3/3, 5/5 and 6.5/8 the respective induced base pressure to initial free-stream static pressure ratios were 5, 8 and 18. (Author).
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 1991 with total page 1460 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis Government-wide Index to Federal Research & Development Reports by :
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Download or read book International Aerospace Abstracts written by and published by . This book was released on 1995 with total page 508 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 1965 with total page 762 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index to Sandia Corporation Publicly Released Reports, 1963-1968 by : Sandia Corporation
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Book Synopsis Comprehensive Dissertation Index by :
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Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :1156 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Book Synopsis Government Reports Annual Index by :
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Book Synopsis Publications of the AIAA by : American Institute of Aeronautics and Astronautics
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Book Synopsis ARS Journal by : American Rocket Society
Download or read book ARS Journal written by American Rocket Society and published by . This book was released on 1962 with total page 2022 pages. Available in PDF, EPUB and Kindle. Book excerpt:
