DTIC ADA145997: An Inviscid Computational Method for pdf

DTIC ADA145997: An Inviscid Computational Method for

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Description of the Book:

An extension to the SWINT code is described which permits inviscid calculations to be performed on the supersonic portion of inlet flow fields. Also described is an interface program which rezones the external flow field applied to several examples. A listing of the extension to SWINT and the interface program are provided in the Appendices along with a set of user instructions and a sample case. (Author

• Creator/s: Defense Technical Information Center
• Date: 3/22/1984
• Year: 1984
• Book Topics/Themes: DTIC Archive, Wardlaw, A B, Jr, NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD, *INVISCID FLOW, *SUPERSONIC INLETS, COMPUTER PROGRAM DOCUMENTATION, COMPUTATIONS, COMPUTER PROGRAMMING, FLOW FIELDS, NOSE TIPS, GUIDED MISSILE COMPONENTS, THREE DIMENSIONAL FLOW

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