Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16
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Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16
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Author : J. S. Hahn
language : en
Publisher:
Release Date : 1972
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16 written by J. S. Hahn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Ablation (Aerothermodynamics) categories.
Technical Abstract Bulletin
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Author :
language : en
Publisher:
Release Date : 1964
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 1964 with Science categories.
Notices Of Changes In Classification Distribution And Availability
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Author :
language : en
Publisher:
Release Date : 1978
Notices Of Changes In Classification Distribution And Availability 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 Science categories.
A Collection Of Technical Papers
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Author :
language : en
Publisher:
Release Date : 1972
A Collection Of Technical Papers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamics categories.
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16
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Author :
language : en
Publisher:
Release Date : 1972
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.
Results are presented from static-force tests and pressure distribution tests of conical bodies with various nose shapes which were chosen to simulate the estimated shapes obtained after significant ablation of the nose had taken place. The basic cone half-angle is 6.3 deg, and the nominal bluntness ratio is 0.25. Nose shapes tested consisted of symmetrical biconics with nose angles of 30, 40, and 50 deg and asymmetrical noses derived from the 50-deg biconic. Results were also obtained for a 50-deg symmetric biconic nose on 4.0- and 9.0-deg cones. The effect of changing the nose-to-cone shoulder radius was investigated on several configurations. Most of the data were obtained at Mach 8, and a limited amount of data was taken at Mach 16. The nominal Reynolds number was 3,100,000 based on the sharp cone length of the 6.3-deg pressure model. For the force tests, the angle-of-attack range was from -5 to 11 deg, and for the pressure tests, the angles of attack included the configuration trim angle and up to 4 deg on either side of the trim angle in increments of generally 1 deg. At Mach 8, data are given for the ablated nose shapes with the vehicle rolled -30, -60, and -90 deg. (Author).
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1982
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 1982 with Science categories.
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1972
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.
Results are presented from static-force tests and pressure distribution tests of conical bodies with various nose shapes which were chosen to simulate the estimated shapes obtained after significant ablation of the nose had taken place. The basic cone half-angle is 6.3 deg, and the nominal bluntness ratio is 0.25. Nose shapes tested consisted of symmetrical biconics with nose angles of 30, 40, and 50 deg and asymmetrical noses derived from the 50-deg biconic. Results were also obtained for a 50-deg symmetric biconic nose on 4.0- and 9.0-deg cones. The effect of changing the nose-to-cone shoulder radius was investigated on several configurations. Most of the data were obtained at Mach 8, and a limited amount of data was taken at Mach 16. The nominal Reynolds number was 3,100,000 based on the sharp cone length of the 6.3-deg pressure model. For the force tests, the angle-of-attack range was from -5 to 11 deg, and for the pressure tests, the angles of attack included the configuration trim angle and up to 4 deg on either side of the trim angle in increments of generally 1 deg. At Mach 8, data are given for the ablated nose shapes with the vehicle rolled -30, -60, and -90 deg. (Author).
Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1990
Government Reports Annual 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 with Government reports announcements & index categories.
Technical Publications Announcements With Indexes
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1962
Technical Publications Announcements With Indexes 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 1962 with Aeronautics categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1980
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 1980 with Aeronautics categories.