Effects of Shock Impingement and Other Factors on Leading-edge Heat Transfer
Author: Dennis M. Bushnell
Publisher:
Published: 1968
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: Dennis M. Bushnell
Publisher:
Published: 1968
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKAuthor: Dennis M. Bushnell
Publisher:
Published: 1968
Total Pages:
ISBN-13:
DOWNLOAD EBOOKAuthor: Holger Babinsky
Publisher: Cambridge University Press
Published: 2011-09-12
Total Pages: 481
ISBN-13: 1139498649
DOWNLOAD EBOOKShock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Author: Michael E. Tauber
Publisher:
Published: 1989
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor: J. Wayne Keyes
Publisher:
Published: 1973
Total Pages: 146
ISBN-13:
DOWNLOAD EBOOKAn analytical and experimental study is presented of the aerodynamic heating resulting from six types of shock interference patterns encountered in high speed flow. Centerline measurements of pressure and heat transfer distributions on basic bodies were obtained in four wind tunnels for Mach numbers from 6 to 20, specific heat ratios from 1.27 to 1.67, and free stream Reynolds numbers from 3 million to 25.6 million per meter. Peak heating and peak pressures up to 17 and 7.5 times stagnation values, respectively, were measured. In general, results obtained from semiempirical methods developed for each of the six types of interference agreed with the experimental peaks.
Author:
Publisher:
Published: 1995
Total Pages: 692
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Published: 1968
Total Pages: 436
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1966
Total Pages: 1464
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1968
Total Pages: 1716
ISBN-13:
DOWNLOAD EBOOKFebruary issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index