Turbulent Reentry
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Turbulent Reentry
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Author : Kyle Fisher
language : en
Publisher: Lulu.com
Release Date :
Turbulent Reentry written by Kyle Fisher and has been published by Lulu.com this book supported file pdf, txt, epub, kindle and other format this book has been release on with categories.
Hypersonic Flows For Reentry Problems
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Author : Jean-Antoine Desideri
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06
Hypersonic Flows For Reentry Problems written by Jean-Antoine Desideri 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 2012-12-06 with Science categories.
This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1992
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 1992 with Aeronautics categories.
Technical Abstract Bulletin
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Author :
language : en
Publisher:
Release Date :
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 with Science categories.
Reentry F Flowfield Solutions At 80 000 Ft
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Author :
language : en
Publisher:
Release Date : 1997
Reentry F Flowfield Solutions At 80 000 Ft 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 categories.
Uniform Roughness Studies
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Author : David Edward Klett
language : en
Publisher:
Release Date : 1992
Uniform Roughness Studies written by David Edward Klett and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Atmospheric turbulence categories.
Juvenile Offending
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Author : Thom Brooks
language : en
Publisher: Taylor & Francis
Release Date : 2023-05-31
Juvenile Offending written by Thom Brooks and has been published by Taylor & Francis this book supported file pdf, txt, epub, kindle and other format this book has been release on 2023-05-31 with Law categories.
Tackling juvenile offending has become a key part of crime reduction strategies. The articles selected for this volume examine juvenile offending from various critical perspectives and represent the work of the most influential international figures in the field. The issues addressed include: the different needs and perspectives of youth offenders; whether offenders should be treated differently from others because of their age; recommendations of policy changes; identification of risk factors; issues surrounding the sentencing of juvenile offenders; and the relevance of restorative justice.
Turbulent Wing Leading Edge Correlation Assessment For The Shuttle Orbiter
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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher: Independently Published
Release Date : 2019-01-13
Turbulent Wing Leading Edge Correlation Assessment For The Shuttle Orbiter written by National Aeronautics and Space Adm Nasa and has been published by Independently Published this book supported file pdf, txt, epub, kindle and other format this book has been release on 2019-01-13 with Science categories.
This study was conducted in support of the Orbiter damage assessment activity that takes place for each Shuttle mission since STS-107 (STS - Space Transportation System). As part of the damage assessment activity, the state of boundary layer (laminar or turbulent) during reentry needs to be estimated in order to define the aerothermal environment on the Orbiter. Premature turbulence on the wing leading edge (WLE) is possible if a surface irregularity promotes early transition and the resulting turbulent wedge flow contaminates the WLE flow. The objective of this analysis is to develop a criterion to determine if and when the flow along the WLE experiences turbulent heating given an incoming turbulent boundary layer that contaminates the attachment line. The data to be analyzed were all obtained as part of the MH-13 Space Shuttle Orbiter Aerothermodynamic Test conducted on a 1.8%-scale Orbiter model at Calspan/University of Buffalo Research Center in the Large Energy National Shock Tunnels facility. A rational framework was used to develop a means to assess the state of the WLE flow on the Orbiter during reentry given a contaminated attachment-line flow. Evidence of turbulent flow on the WLE has been recently documented for a few STS missions during the Orbiter s flight history, albeit late in the reentry trajectory. The criterion developed herein will be compared to these flight results. King, Rudolph A. and Vaughan, Matthew P. Langley Research Center NASA/TM-2009-215949, L-19784, LF99-9713
Numerical Calculation Of The Subsonic And Transonic Turbulent Boundary Layer On An Infinite Yawed Airfoil
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Author : John C. Adams (Jr.)
language : en
Publisher:
Release Date : 1973
Numerical Calculation Of The Subsonic And Transonic Turbulent Boundary Layer On An Infinite Yawed Airfoil written by John C. Adams (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aerodynamics categories.
Hearings
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Author : United States. Congress. House. Committee on Science and Astronautics
language : en
Publisher:
Release Date : 1969
Hearings written by United States. Congress. House. Committee on Science and Astronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.