Dynamic Flight Behavior Of A Ballasted Sphere At Mach Numbers From 0 4 To 14 5
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Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1967
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 1967 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
The Aeronautical Journal
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Author :
language : en
Publisher:
Release Date : 1968
The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aeronautics categories.
Aeronautical Engineering
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Author :
language : en
Publisher:
Release Date : 1993
Aeronautical Engineering written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Aeronautical Engineering A Cumulative Index To A Continuing Bibliography Supplement 287
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Author :
language : en
Publisher:
Release Date : 1993
Aeronautical Engineering A Cumulative Index To A Continuing Bibliography Supplement 287 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with categories.
Aerodynamics Of A Sphere And An Oblate Spheroid For Mach Numbers From 0 6 To 10 5 Including Some Effects Of Test Conditions
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-08-20
Aerodynamics Of A Sphere And An Oblate Spheroid For Mach Numbers From 0 6 To 10 5 Including Some Effects Of Test Conditions 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 2018-08-20 with categories.
Wind-tunnel tests were made for spheres of various sizes over a range of Mach numbers and Reynolds numbers. The results indicated some conditions where the drag was affected by changes in the afterbody pressure due to a shock reflection from the tunnel wall. This effect disappeared when the Mach number was increased for a given sphere size or when the sphere size was decreased for a given Mach number. Drag measurements and Schlieren photographs are presented that show the possibility of obtaining inaccurate data when tests are made with a sphere too large for the test section size and Mach number. Tests were also made of an oblate spheroid. The results indicated a region at high Mach numbers where inherent positive static stability might occur with the oblate-face forward. The drag results are compared with those for a sphere as well as those for various other shapes. The drag results for the oblate spheroid and the sphere are also compared with some calculated results. Spearman, M. Leroy and Braswell, Dorothy O. Langley Research Center RTOP 505-69-20-01...
Aerodynamics Of A Sphere And An Oblate Spheroid For Mach Numbers From 0 6 To 10 5 Including Some Effects Of Test Conditions
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Author : National Aeronautics and Space Administration NASA
language : en
Publisher:
Release Date : 2018-10-23
Aerodynamics Of A Sphere And An Oblate Spheroid For Mach Numbers From 0 6 To 10 5 Including Some Effects Of Test Conditions written by National Aeronautics and Space Administration NASA and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-10-23 with categories.
Wind-tunnel tests were made for spheres of various sizes over a range of Mach numbers and Reynolds numbers. The results indicated some conditions where the drag was affected by changes in the afterbody pressure due to a shock reflection from the tunnel wall. This effect disappeared when the Mach number was increased for a given sphere size or when the sphere size was decreased for a given Mach number. Drag measurements and Schlieren photographs are presented that show the possibility of obtaining inaccurate data when tests are made with a sphere too large for the test section size and Mach number. Tests were also made of an oblate spheroid. The results indicated a region at high Mach numbers where inherent positive static stability might occur with the oblate-face forward. The drag results are compared with those for a sphere as well as those for various other shapes. The drag results for the oblate spheroid and the sphere are also compared with some calculated results. Spearman, M. Leroy and Braswell, Dorothy O. Langley Research Center RTOP 505-69-20-01...
Measurements Of The Mach Number And Pressure On The Afterbody Of A Blunt Nosed Model In Free Flight At Mach Numbers From 6 5 To 14
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Author : Simon C. Sommer
language : en
Publisher:
Release Date : 1960
Measurements Of The Mach Number And Pressure On The Afterbody Of A Blunt Nosed Model In Free Flight At Mach Numbers From 6 5 To 14 written by Simon C. Sommer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamics, Supersonic categories.
Dynamics Of Separating Bodies
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Author : R. D. Turner
language : en
Publisher:
Release Date : 1963
Dynamics Of Separating Bodies written by R. D. Turner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics, Hypersonic categories.
Dynamic models were ejected from the side and base of a carrier vehicle at Mach numbers of 2, 4, 5 and 8. Two capsule shapes were investigated in this program to enable determination of the effects of capsule geometry. The flared capsule confiquration was ballasted in two ways to pro vide two pitch moments of inertia. The cylindrical shape capsule possessed one moment of inertia. The data obtained from these ejections were in the form of high speed motion pictures. The Mach 2, 4, and 5 data were obtained through a Schlieren optical system. The Mach 8 data were obtained with a conventional high speed camera. All 55 data films were analyzed and trajectories are presented. Qualitative descriptions of the dynamic behavior and preliminary quantitative calculations were performed to compare the aerodynamic coefficients obtained from the dynamic tests with those obtained from static tests discussed in Volumes II and III.
Aerodynamics Of A Sphere And An Oblate Spheroid For Mach Numbers From 0 6 To 10 5 Including Some Effects Of Test Conditions
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1993
Aerodynamics Of A Sphere And An Oblate Spheroid For Mach Numbers From 0 6 To 10 5 Including Some Effects Of Test Conditions written by M. Leroy Spearman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aerodynamics categories.
Stability Investigation Of A Blunted Cone And A Blunted Ogive With A Flared Cylinder Afterbody At Mach Numbers From 0 30 To 2 85
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Author : Lucille C. Coltrane
language : en
Publisher:
Release Date : 1962
Stability Investigation Of A Blunted Cone And A Blunted Ogive With A Flared Cylinder Afterbody At Mach Numbers From 0 30 To 2 85 written by Lucille C. Coltrane and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Aircraft categories.