Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7
DOWNLOAD
Download Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7 PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7 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
Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7
DOWNLOAD
Author : Charles R. Rumsey
language : en
Publisher:
Release Date : 1961
Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7 written by Charles R. Rumsey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Fluid mechanics categories.
Inverse Heat Conduction And Heat Exchangers
DOWNLOAD
Author : Suvanjan Bhattacharyya
language : en
Publisher: BoD – Books on Demand
Release Date : 2020-12-02
Inverse Heat Conduction And Heat Exchangers written by Suvanjan Bhattacharyya and has been published by BoD – Books on Demand this book supported file pdf, txt, epub, kindle and other format this book has been release on 2020-12-02 with Science categories.
A direct solution of the heat conduction equation with prescribed initial and boundary conditions yields temperature distribution inside a specimen. The direct solution is mathematically considered as a well-posed one because the solution exists, is unique, and continuously depends on input data. The estimation of unknown parameters from the measured temperature data is known as the inverse problem of heat conduction. An error in temperature measurement, thermal time lagging, thermocouple-cavity, or signal noise data makes stability a problem in the estimation of unknown parameters. The solution of the inverse problem can be obtained by employing the gradient or non-gradient based inverse algorithm. The aim of this book is to analyze the inverse problem and heat exchanger applications in the fields of aerospace, mechanical, applied mechanics, environment sciences, and engineering.
Technical Abstract Bulletin
DOWNLOAD
Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1961-07
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961-07 with Technology categories.
U S Government Research Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1961
U S Government Research 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 1961 with Science categories.
Advances In Computational Heat And Mass Transfer
DOWNLOAD
Author : Ali Cemal Benim
language : en
Publisher: Springer Nature
Release Date : 2024-08-30
Advances In Computational Heat And Mass Transfer written by Ali Cemal Benim and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2024-08-30 with Science categories.
This book reports on cutting-edge applied research and methods in the area of heat and mass transfer and computational fluid dynamics. With a special emphasis on computational methods, it covers applications to different fields, including mechanical engineering, aerospace, and energy, among others. Some relevant experimental validations are described as well. Being the first volume of the two-volume proceedings of the 14th International Conference on Computational Heat and Mass Transfer, ICCHMT 2023, held on September 4-8, 2023, in Düsseldorf, Germany, this book offers a timely perspective of research and applications in the field of computational heat and mass transfer. It also provides both academics and professionals with extensive information and a source of inspiration for new developments and collaborations.
A Collection Of Technical Papers
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1977
A Collection Of Technical Papers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Fluid dynamics categories.
Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1975
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 1975 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.
Measurements Of Aerodynamic Heat Transfer On A 15 Deg Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7
DOWNLOAD
Author : CHARLES B. RUMSEY
language : en
Publisher:
Release Date : 1961
Measurements Of Aerodynamic Heat Transfer On A 15 Deg Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 4 7 written by CHARLES B. RUMSEY and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
Measurements of aerodynamic heat transfer were made at a number of stations along a cone-cylinder-flare model having a 15 degrees total-angle conical nose and a 10 degrees half-angle flare skirt. The maximum Mach number was 4.7, and local Reynolds numbers based on body length to a measurement station varied from 2 x 10 to the 6th power to 138 x 10 to the 6th power. Local Stanton numbers measured on the nose cone and flare showed fair agreement with laminar and turbulent theories, while the measurements on the cylinder were generally somewhat lower than theory. Experimental recovery factors, determined twice during the test, were unaccountably lower than theoretical values. Local transition Reynolds numbers, based on length from the nose tip, varied from 3 x 10 to the 6th power to 18 x 10 to the 6th power and were much lower than values previously obtained on the smoother nose of a similar model. At an angle of attack of about 9 degrees, the heat transfer on the flare increased to more than twie the theoretical turbulent value for zero angle of attack. (Author).
Jet Propulsion
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1961
Jet Propulsion written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Rocketry categories.
Beginning Oct. 1959 some issues include "Russian supplement."
Bibliography Of Scientific And Industrial Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1961
Bibliography Of Scientific And Industrial 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 1961 with Science categories.