Aerodynamic Damping And Oscillatory Stability In Pitch Of A Model Of A Proposed Manned Lifting Entry Vehicle At Mach Numbers Of 1 80 2 16 And 2 86
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The Shock And Vibration Digest
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Author :
language : en
Publisher:
Release Date : 1975
The Shock And Vibration Digest written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Shock (Mechanics) categories.
Aerodynamic Damping And Oscillatory Stability In Pitch Of A Model Of A Proposed Manned Lifting Entry Vehicle At Mach Numbers Of 1 80 2 16 And 2 86
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Author :
language : en
Publisher:
Release Date : 1975
Aerodynamic Damping And Oscillatory Stability In Pitch Of A Model Of A Proposed Manned Lifting Entry Vehicle At Mach Numbers Of 1 80 2 16 And 2 86 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.
Aerodynamic Damping At Mach Numbers Of 1 3 And 1 6 Of A Control Surface On A Two Dimensional Wing By The Free Oscillation Method
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Author : Weimer J. Tuovila
language : en
Publisher:
Release Date : 1960
Aerodynamic Damping At Mach Numbers Of 1 3 And 1 6 Of A Control Surface On A Two Dimensional Wing By The Free Oscillation Method written by Weimer J. Tuovila and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Mach number categories.
Aerodynamic Damping And Oscillatory Stability In Pitch For A Model Of A Typical Subsonic Jet Transport Airplane
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Author : Bruce R. Wright
language : en
Publisher:
Release Date : 1966
Aerodynamic Damping And Oscillatory Stability In Pitch For A Model Of A Typical Subsonic Jet Transport Airplane written by Bruce R. Wright and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Damping (Mechanics) categories.
The Effects Of Static Margin And Rotational Damping In Pitch On The Longitudinal Stability Characteristics Of An Airplane As Determined By Tests Of A Model In The Naca Free Flight Tunnel
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Author : John P. Campbell
language : en
Publisher:
Release Date : 1944
The Effects Of Static Margin And Rotational Damping In Pitch On The Longitudinal Stability Characteristics Of An Airplane As Determined By Tests Of A Model In The Naca Free Flight Tunnel written by John P. Campbell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1944 with Aerodynamics categories.
Summary: The effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane have been determined by flight tests of a model in the NACA free-flight tunnel. In the investigation, the rotational damping in pitch was varied over a wide range by using horizontal tails that varied in area from 0 to 24 percent of the wing area. A range of static margins from 2 to 16 percent of the mean aerodynamic chord was covered in the tests. For each test condition the model was flown and the longitudinal steadiness characteristics were noted. It was found in the investigation that longitudinal steadiness was affected to a much greater extent by changes in static margin than by changes in rotational damping. The best longitudinal steadiness was noted at large values of static margin. For all values of rotational damping, the steadiness of the model decreased as the static margin was reduced. The model was especially unsteady at low values of static margin (0.03 or less). Reduction in rotational damping had little effect on longitudinal steadiness, except that with low values of static margin (0.03 or less) the longitudinal divergences were sometimes more violent with the tailless (low rotational damping) condition.
Aerodynamic Damping At Mach Numbers Of 1 3 And 1 6 Of A Control Surface On A Two Dimensional Wing By A Free Oscillation Method
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Author : W. J. Tuovila
language : en
Publisher:
Release Date : 1956
Aerodynamic Damping At Mach Numbers Of 1 3 And 1 6 Of A Control Surface On A Two Dimensional Wing By A Free Oscillation Method written by W. J. Tuovila and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics, Supersonic categories.
Tests have been made at two supersonic speeds to obtain experimentally the aerodynamic damping characteristics of a control surface on a two-dimensional wing.
Aerodynamic Data Of Space Vehicles
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Author : Claus Weiland
language : en
Publisher: Springer Science & Business Media
Release Date : 2014-02-22
Aerodynamic Data Of Space Vehicles written by Claus Weiland and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-02-22 with Technology & Engineering categories.
The capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.
Wingless Flight
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Author : R. Dale Reed
language : en
Publisher: University Press of Kentucky
Release Date : 2014-07-15
Wingless Flight written by R. Dale Reed and has been published by University Press of Kentucky this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-07-15 with Technology & Engineering categories.
Most lifting bodies, or "flying bathtubs" as they were called, were so ugly only an engineer could love them, and yet, what an elegant way to keep wings from burning off in supersonic flight between earth and orbit. Working in their spare time (because they couldn't initially get official permission), Dale Reed and his team of engineers demonstrated the potential of the design that led to the Space Shuttle. Wingless Flight takes us behind the scenes with just the right blend of technical information and fascinating detail (the crash of M2-F2 found new life as the opening credit for TV's "The Six Million Dollar Man"). The flying bathtub, itself, is finding new life as the proposed escape-pod for the Space Station.
Atmospheric Re Entry Vehicle Mechanics
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Author : Patrick Gallais
language : en
Publisher: Springer Science & Business Media
Release Date : 2007-09-23
Atmospheric Re Entry Vehicle Mechanics written by Patrick Gallais and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2007-09-23 with Technology & Engineering categories.
Based on a long engineering experience, this book offers a comprehensive and state-of-the-art analysis of aerodynamic and flight mechanic entry topics. This updated edition had new chapters on Re-entry on Mars mission, flight quality, rarefied aerodynamics and re-entry accuracy. In addition, it provides a large set of application exercises and solutions.
Handbook Of Supersonic Aerodynamics
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Author : Johns Hopkins University. Applied Physics Laboratory
language : en
Publisher:
Release Date : 1950
Handbook Of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerodynamics, Supersonic categories.