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Accession Number:
ADA010580
Title:
Analysis of Unsteady Transonic Channel Flow with Shock Waves.
Corporate Author:
PURDUE UNIV LAFAYETTE IND PROJECT SQUID HEADQUARTERS
Report Date:
1975-05-01
Abstract:
Inviscid unsteady transonic flow in a two-dimensional channel is analyzed using asymptotic techniques. The analysis includes the case where a shock wave is present in a channel having arbitrary wall shape, with artibrary small disturbances imposed at a given downstream location. Second-order solutions are not uniformly valid near the shock wave, since they do not satisfy the shock jump conditions. It is therefore necessary to obtain inner solutions which are matched asymptotically to those in the outer channel-flow region.
Descriptive Note:
Technical rept.,
Supplementary Note:
Prepared in cooperation with Michigan Univ., Ann Arbor.
Pages:
0041
Contract Number:
N00014-67-A-0226-0005
File Size:
0.00MB
