Full Read and Download Reference eBook
Procedures For Estimating Inlet External And Internal Performance Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Procedures For Estimating Inlet External And Internal Performance book. This book definitely worth reading, it is an incredibly well-written.
Author : B. M. Sharp
Publisher :
Page : 284 pages
File Size : 24,1 MB
Release : 1974
Category : Aerodynamics, Supersonic
ISBN :
Author : Larry K. Ratliff
Publisher :
Page : 164 pages
File Size : 40,9 MB
Release : 1979
Category : Aerodynamics, Supersonic
ISBN :
Author : Paul H. Kutschenreuter
Publisher :
Page : 23 pages
File Size : 43,48 MB
Release : 1963
Category :
ISBN :
The problem of determining performance levels of supersonic/hypersonic combustion inlet models is presented. Previous approaches to this problem are discussed and g40thod involving force balance determination of the internal drag is proposed. Results of a computational procedure formulated for calculating inlet performance levels from measured internal drag values are presented. Effects of chemical reactions and exit flow profile nonuniformity are accounted for. Levels of anticipated accuracy, using this technique, are adequate for present applications over a Mach Number range of 8 to 25. (Author).
Author :
Publisher :
Page : 36 pages
File Size : 47,94 MB
Release : 1961
Category :
ISBN :
Author :
Publisher :
Page : 366 pages
File Size : 31,5 MB
Release : 1989
Category : Airplanes
ISBN :
Author : M. R. Mendenhall
Publisher :
Page : 774 pages
File Size : 36,26 MB
Release : 1992
Category : Guided missiles
ISBN :
Author : Michael J. Hemsch
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 774 pages
File Size : 27,73 MB
Release : 1992
Category : Science
ISBN :
This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
Author :
Publisher :
Page : 444 pages
File Size : 38,45 MB
Release : 1979
Category :
ISBN :
Author :
Publisher :
Page : 452 pages
File Size : 30,1 MB
Release : 2000
Category : Fluid dynamic measurements
ISBN :
Author : Leonard J. Obery
Publisher :
Page : 21 pages
File Size : 13,24 MB
Release : 1957
Category : Aerodynamics, Supersonic
ISBN :
An inlet with combined external and internal compression, formed by spike and cowl oblique shocks, and an over-all length of 2.5 inlet diameters was investigated at Mach numbers from 3.0 to 2.0 over a range of angles of attack. At the design Mach number of 3.0 the low angle cowl, which turned the flow supersonically, generated two internal shocks and focused them on the centerbody surface. These compression waves, with their high pressure gradient, were cancelled by abrupt centerbody turning. This investigation showed that with proper boundary-layer control on the centerbody this method of internal compression did not adversely affect the high performance of the inlet.