Boundary Layer Transition On Cones Near Mach One In An Aeroballistic Range
![Boundary Layer Transition On Cones Near Mach One In An Aeroballistic Range](https://ardhindie.com/assets/pdf.png)
DOWNLOAD
Download Boundary Layer Transition On Cones Near Mach One In An Aeroballistic Range PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Boundary Layer Transition On Cones Near Mach One In An Aeroballistic Range book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Boundary Layer Transition On Cones Near Mach One In An Aeroballistic Range
DOWNLOAD
Author : J. Leith Potter
language : en
Publisher:
Release Date : 1975
Boundary Layer Transition On Cones Near Mach One In An Aeroballistic Range written by J. Leith Potter and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Boundary layer categories.
The feasibility of determining Reynolds numbers of boundary layer transition on sharp, 10-deg, semiangle cones at slightly supersonic free-stream Mach numbers, 1.04 = or
Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1978
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 1978 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.
Applied Mechanics Reviews
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1974
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Mechanics, Applied categories.
Nasa Technical Paper
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1966
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Astronautics categories.
Government Reports Annual Index
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1975
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 1975 with Government reports announcements & index categories.
In Flight Transition Measurement On A 100 Cone At Mach Numbers From 0 5 To 2 0
DOWNLOAD
Author : David F. Fisher
language : en
Publisher:
Release Date : 1982
In Flight Transition Measurement On A 100 Cone At Mach Numbers From 0 5 To 2 0 written by David F. Fisher and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Boundary layer categories.
In Flight Transition Measurement On A 10 Deg Cone At Mach Numbers From 0 5 To 2 0
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1982
In Flight Transition Measurement On A 10 Deg Cone At Mach Numbers From 0 5 To 2 0 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 categories.
Boundary Layer Transition At Supersonic Speeds
DOWNLOAD
Author : E. R. Van Driest
language : en
Publisher:
Release Date : 1961
Boundary Layer Transition At Supersonic Speeds written by E. R. Van Driest and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Supersonic categories.
Experiments carried out in the 12-inch supersonic wind tunnel to investigate the effect of three dimensional roughness elements (spheres) on boundary-layer transition on a 10-degree (apex angle) cone without heat transfer are described. The local Mach number for these tests was 2.71. The data show clearly that the minimum (effective) size of trip required to bring transition to its lowest Reynolds number varies power of the distance from the apex of the cone to the trip. Use of available data at other Mach numbers indicates that the Mach number influence for effective tripping is taken into account by a simple expression. Some remarks concerning the roughness variation for transition on a blunt body are made. Finally, a general criterion is introduced which gives insight to the transition phenomenon and anticipates effects of external and internal disturbances, Mach number transfer.
Agard Advisory Report
DOWNLOAD
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
language : en
Publisher:
Release Date : 1988
Agard 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 1988 with Aerodynamics categories.
A Review Of High Speed Convective Heat Transfer Computation Methods
DOWNLOAD
Author : Michael E. Tauber
language : en
Publisher:
Release Date : 1989
A Review Of High Speed Convective Heat Transfer Computation Methods written by Michael E. Tauber and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aerodynamic heating categories.