An edge-based solution-adaptive method applied to the AIRPLANE code /

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Bibliographic Details
Main Author: Biswas, R. (Rupak)
Corporate Author: Research Institute for Advanced Computer Science (U.S.)
Other Authors: Thomas, Scott D., Cliff, Susan E.
Format: Government Document Book
Language:English
Published: [Moffett Field, Calif.] : [Springfield, Va.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [National Technical Information Service, distributor], [1995]
Series:RIACS technical report TR 95-22.
NASA contractor report ; NASA CR-199754.
Subjects:

MARC

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260 |a [Moffett Field, Calif.] :  |b Research Institute for Advanced Computer Science, NASA Ames Research Center ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c [1995] 
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650 7 |a Aircraft configurations.  |2 nasat 
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650 7 |a Pressure distribution.  |2 nasat 
650 7 |a Shock waves.  |2 nasat 
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650 7 |a Supersonic flow.  |2 nasat 
650 7 |a Transonic flow.  |2 nasat 
650 7 |a Unstructured grids (Mathematics)  |2 nasat 
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700 1 |a Cliff, Susan E. 
710 2 |a Research Institute for Advanced Computer Science (U.S.) 
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