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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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.
Measurements Of Aerodynamic Heat Transfer And Boundary Layer Transition On A 150 Cone In Free Flight At Supersonic Mach Numbers Up To 5 2
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Author : Charles B. Rumsey
language : en
Publisher:
Release Date : 1961
Measurements Of Aerodynamic Heat Transfer And Boundary Layer Transition On A 150 Cone In Free Flight At Supersonic Mach Numbers Up To 5 2 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 1961 with Aerodynamic load categories.
Abstract:
Measurements Of Aerodynamic Heat Transfer And Boundary Layer Transition On A 10 Cone In Free Flight At Supersonic Mach Numbers Up To 5 9
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Author : Charles B. Rumsey
language : en
Publisher:
Release Date : 1956
Measurements Of Aerodynamic Heat Transfer And Boundary Layer Transition On A 10 Cone In Free Flight At Supersonic Mach Numbers Up To 5 9 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 1956 with Aerodynamics categories.
Abstract: Aerodynamic heat-transfer measurements were at six stations on the 40-inch-long 10° total-angle conical nose of a rocket-propelled model which was flight tested at Mach numbers up to 5.9. The range of local Reynolds number was from 6.6 x 106 to 55.2 x 106. Laminar, transitional, and turbulent heat-transfer coefficients were measured, and, in general, the laminar and turbulent measurements were in good agreement with theory for cones. Experimental transition Reynolds numbers varied from less than 8.5 x 106 to 19.4 x 106. At a relatively constant ratio of wall temperature to local static temperature near 1.2, the transition Reynolds number increased from 9.2 x 106 to 19.4 x 106 as Mach number increased from 1.57 to 3.38. At Mach numbers near 3.7, the transition Reynolds number decreased as the skin temperature increased toward adiabatic wall temperatures.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1961
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 1961 with categories.
Measurements Of Aerodynamic Heat Transfer And Boundary Layer Transition On A 10 Degree Cone In Free Flight At Supersonic Mach Numbers Up To 5 9
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Author : Charles B. Rumsey
language : en
Publisher:
Release Date : 1961
Measurements Of Aerodynamic Heat Transfer And Boundary Layer Transition On A 10 Degree Cone In Free Flight At Supersonic Mach Numbers Up To 5 9 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 1961 with Heat categories.
Free Flight Aerodynamic Heating Data To Mach Number 10 4 For A Modified Von Karman Nose Shape
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Author :
language : en
Publisher:
Release Date : 1961
Free Flight Aerodynamic Heating Data To Mach Number 10 4 For A Modified Von Karman Nose Shape 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.
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 : Langley Aeronautical Laboratory
language : en
Publisher: Hassell Street Press
Release Date : 2021-09-10
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 Langley Aeronautical Laboratory and has been published by Hassell Street Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2021-09-10 with categories.
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Nasa Technical Report
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Author :
language : en
Publisher:
Release Date : 1961
Nasa Technical Report 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 Aerodynamics categories.
Monthly Catalog Of United States Government Publications
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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1960
Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Government publications categories.
Technical Abstract Bulletin
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language : en
Publisher:
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Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.