Experimental Investigation Of The Flow Field And Heat Transfer Over The Apollo Capsule Afterbody At A Mach Number Of 20


Experimental Investigation Of The Flow Field And Heat Transfer Over The Apollo Capsule Afterbody At A Mach Number Of 20
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Experimental Investigation Of The Flow Field And Heat Transfer Over The Apollo Capsule Afterbody At A Mach Number Of 20


Experimental Investigation Of The Flow Field And Heat Transfer Over The Apollo Capsule Afterbody At A Mach Number Of 20
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Author :
language : en
Publisher:
Release Date : 1965

Experimental Investigation Of The Flow Field And Heat Transfer Over The Apollo Capsule Afterbody At A Mach Number Of 20 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.




The Effect Of Protuberances Cavities And Angle Of Attack On The Wind Tunnel Pressure And Heat Transfer Distribution For The Apollo Command Module


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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Author : John J. Bertin
language : en
Publisher:
Release Date : 1966

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.




Heat Transfer Rate And Pressure Measurements Obtained During Apollo Orbital Entries


Heat Transfer Rate And Pressure Measurements Obtained During Apollo Orbital Entries
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Author : Dorothy B. Lee
language : en
Publisher:
Release Date : 1970

Heat Transfer Rate And Pressure Measurements Obtained During Apollo Orbital Entries written by Dorothy B. Lee and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Apollo (Gardolo di Trento, Italy) categories.




Nasa Technical Memorandum


Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1966

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aeronautics categories.




Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1971

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.




Shock Waves


Shock Waves
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Author : Klaus Hannemann
language : en
Publisher: Springer Science & Business Media
Release Date : 2009-04-01

Shock Waves written by Klaus Hannemann and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2009-04-01 with Science categories.


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.



Experimental Investigation Of Flow Characteristics Of The Apollo Reentry Configuration At A Mach Number Of 20 In Nitrogen


Experimental Investigation Of Flow Characteristics Of The Apollo Reentry Configuration At A Mach Number Of 20 In Nitrogen
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Author :
language : en
Publisher:
Release Date : 1966

Experimental Investigation Of Flow Characteristics Of The Apollo Reentry Configuration At A Mach Number Of 20 In Nitrogen written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.




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


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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Author :
language : en
Publisher:
Release Date : 1965

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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.




Heat Transfer And Pressure Distributions On Apollo Models At M


Heat Transfer And Pressure Distributions On Apollo Models At M
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Author :
language : en
Publisher:
Release Date : 1965

Heat Transfer And Pressure Distributions On Apollo Models At M written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.




04 2370 04 2473


04 2370 04 2473
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Author :
language : en
Publisher:
Release Date : 2004

04 2370 04 2473 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2004 with Thermodynamics categories.