Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : Program documentation and test case

Author:: Mcmillan, O. J.
Published:: Jun 1, 1981.
Physical Description:: 1 electronic document
Additional Creators:: Biringen, S.

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Summary:

The source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented.

Other Subject(s):

AERODYNAMICS

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19810017541.
Accession ID: 81N26077.
NEAR-TR-233.
NASA-CR-3414.

Terms of Use and Reproduction:

No Copyright.

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