Three-dimensional viscous design methodology for advanced technology aircraft supersonic inlet systemsA broad program to develop advanced, reliable, and user oriented three-dimensional viscous design techniques for supersonic inlet systems, and encourage their transfer into the general user community is discussed. Features of the program include: (1) develop effective methods of computing three-dimensional flows within a zonal modeling methodology; (2) ensure reasonable agreement between said analysis and selective sets of benchmark validation data; (3) develop user orientation into said analysis; and (4) explore and develop advanced numerical methodology. Previously announced in STAR as N84-13190
Document ID
19840038503
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, B. H. (NASA Lewis Research Center Cleveland, OH, United States)