Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model
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Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model
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Author : C. F. Lo
language : en
Publisher:
Release Date : 1973
Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model written by C. F. Lo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aerofoils categories.
The transonic scaling effect of shock wave/boundary-layer interaction on a quasi, two-dimensional C-141 airfoil was investigated. Data were obtained from the AEDC Propulsion Wind Tunnel Facility Aerodynamic Wind Tunnel (4T) and Propulsion Wind Tunnel (16T) and from the NASA Marshall Space FLIGHT Center High Reynolds Number Tunnel with 6-in.- and 24-in.-chord airfoils for a range 0.70 to 0.85. In addition to the investigation of the effect of Reynolds number on the airfoil pressure distribution, the effect of fixed boundary-layer transition was evaluated using grit-type transition strips on the airfoil surface. The significant parameters affecting the shock wave/boundary-layer interaction are identified. The data indicate that simulation of higher Reynolds number data on the C-141 airfoil model is feasible by use of a fixed-boundary-layer-transition strip. (Author).
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1973
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 1973 with Aeronautics categories.
Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model
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Author :
language : en
Publisher:
Release Date : 1973
Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.
The transonic scaling effect of shock wave/boundary-layer interaction on a quasi, two-dimensional C-141 airfoil was investigated. Data were obtained from the AEDC Propulsion Wind Tunnel Facility Aerodynamic Wind Tunnel (4T) and Propulsion Wind Tunnel (16T) and from the NASA Marshall Space FLIGHT Center High Reynolds Number Tunnel with 6-in.- and 24-in.-chord airfoils for a range 0.70 to 0.85. In addition to the investigation of the effect of Reynolds number on the airfoil pressure distribution, the effect of fixed boundary-layer transition was evaluated using grit-type transition strips on the airfoil surface. The significant parameters affecting the shock wave/boundary-layer interaction are identified. The data indicate that simulation of higher Reynolds number data on the C-141 airfoil model is feasible by use of a fixed-boundary-layer-transition strip. (Author).
Evaluation Of A Method For Computation Of Separated Turbulent Compressible Boundary Layers
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Author : M. C. Altstatt
language : en
Publisher:
Release Date : 1976
Evaluation Of A Method For Computation Of Separated Turbulent Compressible Boundary Layers written by M. C. Altstatt and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Compressibility categories.
A computer code for a turbulent, compressible boundary-layer method, capable of carrying out computations in a region of separated flow, is developed and tested. The procedure after separation is to specify either friction velocity or boundary-layer thickness as an independent variable and obtain external velocity as a dependent variable. This requires a trial and error alternation of the specified variable in order to match the desired experimental or computed external velocity. Satisfactorily results were obtained by this method in the analysis of certain specialized cases of separated flow. (Author).
Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model
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Author :
language : en
Publisher:
Release Date : 1973
Transonic Scaling Effect On A Quasi Two Dimensional C 141 Airfoil Model written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.
The transonic scaling effect of shock wave/boundary-layer interaction on a quasi, two-dimensional C-141 airfoil was investigated. Data were obtained from the AEDC Propulsion Wind Tunnel Facility Aerodynamic Wind Tunnel (4T) and Propulsion Wind Tunnel (16T) and from the NASA Marshall Space FLIGHT Center High Reynolds Number Tunnel with 6-in.- and 24-in.-chord airfoils for a range 0.70 to 0.85. In addition to the investigation of the effect of Reynolds number on the airfoil pressure distribution, the effect of fixed boundary-layer transition was evaluated using grit-type transition strips on the airfoil surface. The significant parameters affecting the shock wave/boundary-layer interaction are identified. The data indicate that simulation of higher Reynolds number data on the C-141 airfoil model is feasible by use of a fixed-boundary-layer-transition strip. (Author).
Technical Information Indexes
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Author : United States. Naval Air Systems Command
language : en
Publisher:
Release Date : 1974
Technical Information Indexes written by United States. Naval Air Systems Command and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics, Military categories.
Aeronautical Engineering
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Author :
language : en
Publisher:
Release Date : 1992
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 1992 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).
Agard Advisory Report
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Author :
language : en
Publisher:
Release Date : 1975
Agard Advisory Report 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 Aerodynamics categories.
Advisory Report
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Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
language : en
Publisher:
Release Date : 1975
Advisory Report written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aeronautics categories.
Government Reports Announcements
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Author :
language : en
Publisher:
Release Date : 1973-08-10
Government Reports Announcements written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973-08-10 with Technology categories.