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
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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
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Author : Jerome D. Julius
language : en
Publisher:
Release Date : 1959
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
Aerospace Engineering Index
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Author :
language : en
Publisher:
Release Date : 1958
Aerospace Engineering Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with categories.
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
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Author : Jerome D. Julius
language : en
Publisher:
Release Date : 1959
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
Measurements Of Pressure And Local Heat Transfer On A 20 Cone At Angles Of Attack Up To 20 For A Mach Number 0f 4 95
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Author : Jerome D. Julius
language : en
Publisher:
Release Date : 1959
Measurements Of Pressure And Local Heat Transfer On A 20 Cone At Angles Of Attack Up To 20 For A Mach Number 0f 4 95 written by Jerome D. Julius and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
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
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Author :
language : en
Publisher:
Release Date : 1959
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
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
DOWNLOAD
Author : Jerome D. Julius
language : en
Publisher:
Release Date : 1959
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
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
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Author : Raul Jorge Conti
language : en
Publisher:
Release Date : 1961
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Heat categories.
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.
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
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Author : RAUL J. CONTI
language : en
Publisher:
Release Date : 1961
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
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).
Free Flight Measurements Of Aerodynamic Heat Transfer To Mach Number 3 9 And Of Drag To Mach Number 6 9 Of A Fin Stabilized Cone Cylinder Configuration
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Author : Charles B. Rumsey
language : en
Publisher:
Release Date : 1955
Free Flight Measurements Of Aerodynamic Heat Transfer To Mach Number 3 9 And Of Drag To Mach Number 6 9 Of A Fin Stabilized Cone Cylinder Configuration written by Charles B. Rumsey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aerodynamic heating categories.
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
Heat Transfer And Pressure Measurements Of A 1 7 Scale Model Of A Mercury Capsule At Angles Of Attack From 3 Deg To Or 20 Deg At Mach Numbers Of 3 50 And 4 44
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Author :
language : en
Publisher:
Release Date : 1961
Heat Transfer And Pressure Measurements Of A 1 7 Scale Model Of A Mercury Capsule At Angles Of Attack From 3 Deg To Or 20 Deg At Mach Numbers Of 3 50 And 4 44 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.