Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14

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language : en
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Release Date : 1975
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Release Date : 1966
Government Wide Index To Federal Research Development 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 1966 with Government publications categories.
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Author : United States. Air Force. Office of Aerospace Research
language : en
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Release Date : 1967
Oar Quarterly Index Of Current Research Results written by United States. Air Force. Office of Aerospace Research and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aeronautics, Military categories.
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language : en
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Release Date : 1967
U S Government Research Development 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 1967 with Science categories.
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Oar Index Of Research Results
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Author :
language : en
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Release Date : 1967
Oar Index Of Research Results written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aeronautics categories.
Oar Cumulative Index Of Research Results
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Author : United States. Air Force. Office of Aerospace Research
language : en
Publisher:
Release Date : 1965
Oar Cumulative Index Of Research Results written by United States. Air Force. Office of Aerospace Research and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aeronautics categories.
Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14
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Author : Stuart E. Larsen
language : en
Publisher:
Release Date : 1965
Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14 written by Stuart E. Larsen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamic load categories.
Two slender cones, L/D = 4 and L/D = 8, were tested at a nominal Mach number of 14 in air. Total pressure and temperature conditions were 1400-1600 psia and 1350-1550F., respectively. Experimental pressure data was obtained for angles of attack between 0-20 degrees and circumferential angles of 0-180 degrees. This data is presented in conjunction with Sims' and Newtonian Impact theories. (Author).