Accession Number : AD0783297
Title : A Multi-Stream Compressible Flow Computerized Analysis.
Descriptive Note : Interim rept.,
Corporate Author : UNITED AIRCRAFT RESEARCH LABS EAST HARTFORD CONN
Personal Author(s) : Cohen,L. S. ; Flaherty,R. J.
Report Date : MAY 1974
Pagination or Media Count : 45
Abstract : A description of a FORTRAN 5 computer code for predicting the inviscid flow field produced by the interaction between several adjacent streams is presented. The flow field solution is based on the method of characteristics. To illustrate the use of the code, analytical results are used to develop optical property predictions for both the near and far fields for centrifugal aerowindow flow fields generated by four, two, and single nozzles. Further, a comparison is made between the four nozzle aerowindow far field optical predictions and experimental results. All instructions needed for execution of the computer program are contained within. (Author)
Descriptors : *Compressible flow, *Laser cavities, *Flow fields, Laser beams, Nozzle gas flow, Shock waves, Flow visualization, FORTRAN, Far field, Computer programming
Subject Categories : Lasers and Masers
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE