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Pressure And Heat Transfer Measurements On The Flat Face Of A Blunted 10 Degree Half Cone Body Semidisk At A Mach Number Of 615
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Book Synopsis Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15 by : P. Calvin Stainback
Download or read book Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15 written by P. Calvin Stainback and published by . This book was released on 1963 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15 by : P. Calvin Stainback
Download or read book Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15 written by P. Calvin Stainback and published by . This book was released on 1963 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° by : Raul Jorge Conti
Download or read book Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° written by Raul Jorge Conti and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.
Book Synopsis Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 by : Jerome D. Julius
Download or read book Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees by : James L. Amick
Download or read book Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees written by James L. Amick and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ by : Dennis M. Bushnell
Download or read book Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ written by Dennis M. Bushnell and published by . This book was released on 1968 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 by : J. David Dearing
Download or read book Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 written by J. David Dearing and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 by : Peter F. Intrieri
Download or read book Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 written by Peter F. Intrieri and published by . This book was released on 1962 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References] by :
Download or read book Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References] written by and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Pressure and Local Heat Transfer on a 20 Deg Cone at Angles of Attack Up to 20 Deg for a Mach Number of 4.95 by :
Download or read book Measurements of Pressure and Local Heat Transfer on a 20 Deg Cone at Angles of Attack Up to 20 Deg for a Mach Number of 4.95 written by and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Pressures, Heat Transfer, and Surface Flow Patterns Around a Blunt Half-cone Lifting Reentry Body at a Mach Number of 9.6 by :
Download or read book Experimental Investigation of the Pressures, Heat Transfer, and Surface Flow Patterns Around a Blunt Half-cone Lifting Reentry Body at a Mach Number of 9.6 written by and published by . This book was released on 1961 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg by :
Download or read book Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1967 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees by : Dennis M. Bushnell
Download or read book Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees written by Dennis M. Bushnell and published by . This book was released on 1968 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Pressure and Local Heat Transfer on a 20 Degree Cone at Angles of Attack Up to 20 Degrees for a Mach Number of 4.95 by : Jerome D. Julius
Download or read book Measurements of Pressure and Local Heat Transfer on a 20 Degree Cone at Angles of Attack Up to 20 Degrees for a Mach Number of 4.95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat-transfer and Pressure Measurement at a Mach Number of 6 on Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° by : Raul J. Conti
Download or read book Laminar Heat-transfer and Pressure Measurement at a Mach Number of 6 on Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° written by Raul J. Conti and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on Sharp and Blunt 15 Degree Half-angle Cones at Angles of Attack Up to 90 Degrees by : RAUL J. CONTI
Download or read book Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on Sharp and Blunt 15 Degree Half-angle Cones at Angles of Attack Up to 90 Degrees written by RAUL J. CONTI and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer and pressure distributions were measured on sharp and blunt 15 degree half-angle cones. The flow was near conical on the windward side of the models up to an angle of attack of about 60 degrees. At angles of attack above 70 degrees the flow departed noticeably from conical characteristics. Heat-transfer and pressure measurements were found to agree satisfactorily with theories of simple application. At large angles of attack the effects of nose bluntness are very small in the region beyond two nose radii from the point of tangency. (Author).
Download or read book สภานิติบัญญัติแห่งชาติ written by and published by . This book was released on 2007 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: