An edge-based solution-adaptive method applied to the AIRPLANE code
By: Rupak Biswas, Scott D. Thomas, Susan E. Cliff.
Contributors: Thomas, Scott D.; Cliff, Susan E.; Research Institute for Advanced Computer Science (U.S.)
Series: NASA contractor report -- NASA CR-199754.; RIACS technical report -- 95.22.; RIACS technical report -- TR 95-22.
Publisher: Research Institute for Advanced Computer Science, NASA Ames Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: [Moffett Field, CA]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft configurations.; Flow distribution.; Grid generation (Mathematics); Near fields.; Pressure distribution.; Shock waves.; Sonic booms.; Supersonic flow.; Transonic flow.; Unstructured grids (Mathematics)
Other titles: Edge based solution adaptive method applied to the AIRPLANE code.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0197-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.