Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07
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Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07
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Author : Robert L. O'Neal
language : en
Publisher:
Release Date : 1962
Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07 written by Robert L. O'Neal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Heat categories.
Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07
Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1963
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Mechanics, Applied 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.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1990-07
Government Reports Announcements 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 1990-07 with Science categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1997
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Aeronautics categories.
Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07
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Author : Robert L. O'Neal
language : en
Publisher:
Release Date : 1958
Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07 written by Robert L. O'Neal 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.
Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07
DOWNLOAD
Author : Robert L. O'Neal
language : en
Publisher:
Release Date : 1962
Heat Transfer To 0 Degree And 75 Degree Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07 written by Robert L. O'Neal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Heat categories.
Heat Transfer To 0 Degree And 75 Degrees Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07
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Author : ROBERT L. O'NEAL
language : en
Publisher:
Release Date : 1962
Heat Transfer To 0 Degree And 75 Degrees Swept Blunt Leading Edges In Free Flight At Mach Numbers From 1 90 To 3 07 written by ROBERT L. O'NEAL and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with categories.
A flight investigation of a rocket-powered model was conducted to study the heat transfer to wing leading edges in the vicinity of their juncture with a cylindrical body. Heat-transfer data were obtained on leading edges of 3/4-inch diameter at sweep angles of 0 and 75 degrees, Mach numbers from 1.90 to 3.07, and Reynolds numbers based on leading-edge diameter from 8.05 to 11.80 times 10 to the 5th power. The measured heating rates of both the 0 and 75 degrees swept leading edges were of the magnitude predicted by turbulent theory rather than by laminar theory. It is believed that the high level of heating observed on the leading edges was due to the influence of conditions existing in the turbulent boundary layer of the body. Comparison of the average measured heating on the cylindrical portions of both the swept and unswept leading edges indicates that the heating of the unswept segment was generally about twice that of the swept segment. (Author).
Popular Mechanics
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Author :
language : en
Publisher:
Release Date : 2000-01
Popular Mechanics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000-01 with categories.
Popular Mechanics inspires, instructs and influences readers to help them master the modern world. Whether it’s practical DIY home-improvement tips, gadgets and digital technology, information on the newest cars or the latest breakthroughs in science -- PM is the ultimate guide to our high-tech lifestyle.