Experimental Investigation of the Flow Field and Heat Transfer Over the Apollo-capsule Afterbody at a Mach Number of 20

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of the Flow Field and Heat Transfer Over the Apollo-capsule Afterbody at a Mach Number of 20 by :

Download or read book Experimental Investigation of the Flow Field and Heat Transfer Over the Apollo-capsule Afterbody at a Mach Number of 20 written by and published by . This book was released on 1965 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of the Overall Pressure Distribution, Flow Field, and Afterbody Heat Transfer Distribution of an Apollo Reentry Configuration at a Mach Number of 8

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of the Overall Pressure Distribution, Flow Field, and Afterbody Heat Transfer Distribution of an Apollo Reentry Configuration at a Mach Number of 8 by :

Download or read book Experimental Investigation of the Overall Pressure Distribution, Flow Field, and Afterbody Heat Transfer Distribution of an Apollo Reentry Configuration at a Mach Number of 8 written by and published by . This book was released on 1963 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 440 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1971 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1966 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Free-flight Investigation of the Heat Transfer and Afterbody Flow Field of an Apollo-type Configuration at Speeds to 10,000 Ft/sec

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Free-flight Investigation of the Heat Transfer and Afterbody Flow Field of an Apollo-type Configuration at Speeds to 10,000 Ft/sec by :

Download or read book A Free-flight Investigation of the Heat Transfer and Afterbody Flow Field of an Apollo-type Configuration at Speeds to 10,000 Ft/sec written by and published by . This book was released on 1963 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Flow Characteristics of the Apollo Reentry Configuration at a Mach Number of 20 in Nitrogen

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of Flow Characteristics of the Apollo Reentry Configuration at a Mach Number of 20 in Nitrogen by :

Download or read book Experimental Investigation of Flow Characteristics of the Apollo Reentry Configuration at a Mach Number of 20 in Nitrogen written by and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Rate and Pressure Measurements Obtained During Apollo Orbital Entries

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer Rate and Pressure Measurements Obtained During Apollo Orbital Entries by : Dorothy B. Lee

Download or read book Heat-transfer Rate and Pressure Measurements Obtained During Apollo Orbital Entries written by Dorothy B. Lee and published by . This book was released on 1970 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of the Apollo Afterbody Pressure and Heat Transfer at High Enthalpy

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Investigation of the Apollo Afterbody Pressure and Heat Transfer at High Enthalpy by :

Download or read book An Investigation of the Apollo Afterbody Pressure and Heat Transfer at High Enthalpy written by and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effect of Protuberances, Cavities, and Angle of Attack on the Wind-tunnel Pressure and Heat-transfer Distribution for the Apollo Command Module

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis The Effect of Protuberances, Cavities, and Angle of Attack on the Wind-tunnel Pressure and Heat-transfer Distribution for the Apollo Command Module by : John J. Bertin

Download or read book The Effect of Protuberances, Cavities, and Angle of Attack on the Wind-tunnel Pressure and Heat-transfer Distribution for the Apollo Command Module written by John J. Bertin and published by . This book was released on 1966 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer and Pressure Distributions on Apollo Models at M

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat-transfer and Pressure Distributions on Apollo Models at M by :

Download or read book Heat-transfer and Pressure Distributions on Apollo Models at M written by and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the Heat Transfer and Fluid Mechanics Institute

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ISBN 13 :
Total Pages : 490 pages
Book Rating : 4.:/5 (4 download)

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Book Synopsis Proceedings of the Heat Transfer and Fluid Mechanics Institute by : Heat Transfer and Fluid Mechanics Institute

Download or read book Proceedings of the Heat Transfer and Fluid Mechanics Institute written by Heat Transfer and Fluid Mechanics Institute and published by . This book was released on 1967 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Telemetry Measurements of Afterbody Pressures on Free-flying Models of the Apollo Capsule at Mach Numbers from 10 to 21 in Helium and 14 in Air

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Telemetry Measurements of Afterbody Pressures on Free-flying Models of the Apollo Capsule at Mach Numbers from 10 to 21 in Helium and 14 in Air by :

Download or read book Telemetry Measurements of Afterbody Pressures on Free-flying Models of the Apollo Capsule at Mach Numbers from 10 to 21 in Helium and 14 in Air written by and published by . This book was released on 1965 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock Waves

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Publisher : Springer Science & Business Media
ISBN 13 : 3540851682
Total Pages : 810 pages
Book Rating : 4.5/5 (48 download)

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Book Synopsis Shock Waves by : Klaus Hannemann

Download or read book Shock Waves written by Klaus Hannemann and published by Springer Science & Business Media. This book was released on 2009-04-01 with total page 810 pages. Available in PDF, EPUB and Kindle. Book excerpt: The 26th International Symposium on Shock Waves in Göttingen, Germany was jointly organised by the German Aerospace Centre DLR and the French-German Research Institute of Saint Louis ISL. The year 2007 marked the 50th anniversary of the Symposium, which first took place in 1957 in Boston and has since become an internationally acclaimed series of meetings for the wider Shock Wave Community. The ISSW26 focused on the following areas: Shock Propagation and Reflection, Detonation and Combustion, Hypersonic Flow, Shock Boundary Layer Interaction, Numerical Methods, Medical, Biological and Industrial Applications, Richtmyer Meshkov Instability, Blast Waves, Chemically Reacting Flows, Diagnostics, Facilities, Flow Visualisation, Ignition, Impact and Compaction, Multiphase Flow, Nozzles Flows, Plasmas and Propulsion. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 26 and individuals interested in these fields.

04-2370 - 04-2473

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ISBN 13 :
Total Pages : 530 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 04-2370 - 04-2473 by :

Download or read book 04-2370 - 04-2473 written by and published by . This book was released on 2004 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Free-flight Investigation of Heat Transfer to an Unswept Cylinder Subjected to an Incident Shock and Flow Interference from an Upstream Body at Mach Numbers Up to 5.50

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Free-flight Investigation of Heat Transfer to an Unswept Cylinder Subjected to an Incident Shock and Flow Interference from an Upstream Body at Mach Numbers Up to 5.50 by : Howard S. Carter

Download or read book Free-flight Investigation of Heat Transfer to an Unswept Cylinder Subjected to an Incident Shock and Flow Interference from an Upstream Body at Mach Numbers Up to 5.50 written by Howard S. Carter and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer rates have been measured in free flight along the stagnation line of an unswept cylinder mounted transversely on an axial cylinder so that the shock wave from the hemispherical nose of the axial cylinder intersected the bow shock of the unswept transverse cylinder. Data were obtained at Mach numbers from 2.53 to 5.50 and at Reynolds numbers based on the transverse cylinder diameter from 1.00 x 106 to 1.87 x 106. Shadowgraph pictures made in a wind tunnel showed that the flow field was influenced by boundary-layer separation on the axial cylinder and by end effects on the transverse cylinder as well as by the intersecting shocks. Under these conditions, the measured heat-transfer rates had inconsistent variations both in magnitude and distribution which precluded separating the effects of these disturbances. The general magnitude of the measured heating rates at Mach numbers up to 3 was from 0.1 to 0.5 of the theoretical laminar heating rates along the stagnation line for an infinite unswept cylinder in undisturbed flow. At Mach numbers above 4 the measured heating rates were from 1.5 to 2 times the theoretical rates.

An Experimental Investigation at a Mach Number of 4.95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined with the Free-stream Velocity

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An Experimental Investigation at a Mach Number of 4.95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined with the Free-stream Velocity by : P. Calvin Stainback

Download or read book An Experimental Investigation at a Mach Number of 4.95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined with the Free-stream Velocity written by P. Calvin Stainback and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Journal of Thermophysics and Heat Transfer

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ISBN 13 :
Total Pages : 996 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Journal of Thermophysics and Heat Transfer by :

Download or read book Journal of Thermophysics and Heat Transfer written by and published by . This book was released on 2006 with total page 996 pages. Available in PDF, EPUB and Kindle. Book excerpt: This journal is devoted to the advancement of the science and technology of thermophysics and heat transfer through the dissemination of original research papers disclosing new technical knowledge and exploratory developments and applications based on new knowledge. It publishes papers that deal with the properties and mechanisms involved in thermal energy transfer and storage in gases, liquids, and solids or combinations thereof. These studies include conductive, convective, and radiative modes alone or in combination and the effects of the environment.