Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Deg Near Flight Conditions At Mach 7
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Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Deg Near Flight Conditions At Mach 7
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-08-22
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Deg Near Flight Conditions At Mach 7 written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-08-22 with categories.
Heat transfer rates and pressures were obtained on an elevon plate (deflected 30 deg) and a flat plate upstream of the elevon in an 8 foot high-temperature structures tunnel. The flight Reynolds number and flight total enthalpy for altitudes of 26.8 km and 28.7 km at Mach seven were duplicated. The heat transfer and pressure data were used to establish heating and pressure loads. The measured heating was compared with several theoretical predictions, and the closest agreement obtained with a Schultz-Grunow reference enthalpy method of calculation. Johnson, C. B. and Taylor, A. H. and Weinstein, I. Langley Research Center NASA-TM-X-3563, L-11524 RTOP 505-11-31-02...
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Deg Near Flight Conditions At Mach 7
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Author : C. B. Johnson
language : en
Publisher:
Release Date : 1977
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Deg Near Flight Conditions At Mach 7 written by C. B. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with categories.
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Near Flight Conditions At Mach 7
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Author : Charles B. Johnson
language : en
Publisher:
Release Date : 1977
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Near Flight Conditions At Mach 7 written by Charles B. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Aeronautics, Hypersonic categories.
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Near Flight Conditions At Mach 7
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Author : Charles B. Johnson
language : en
Publisher:
Release Date : 1977
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 Near Flight Conditions At Mach 7 written by Charles B. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with categories.
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 N Ear Flight Conditions At Mach 7
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Author : Charles B. Johnson
language : en
Publisher:
Release Date : 1977
Heat Transfer And Pressure Measurements On A Simulated Elevon Deflected 30 N Ear Flight Conditions At Mach 7 written by Charles B. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Heat categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1977
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Aeronautics categories.
Evaluation Of Three Thermal Protection Systems In A Hypersonic High Heating Rate Environment Induced By An Elevon Deflected 30 Deg
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Author :
language : en
Publisher:
Release Date : 1977
Evaluation Of Three Thermal Protection Systems In A Hypersonic High Heating Rate Environment Induced By An Elevon Deflected 30 Deg written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with categories.
Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Deg Swept Double Delta Wing At Mach Numbers From 0 80 To 1 20 With Summary Of Data From 0 20 To 6 0
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Author :
language : en
Publisher:
Release Date : 1979
Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Deg Swept Double Delta Wing At Mach Numbers From 0 80 To 1 20 With Summary Of Data From 0 20 To 6 0 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with categories.
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1978
Nasa Sp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Aeronautics 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 : 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.