Steady and unsteady three-dimensional transonic flow computations by integral equation method
Subtitle: final technical report
By: by Hong Hu, principal investigator.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-196777.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Computer systems performance.; Integral equations.; Massively parallel processors.; Navier-Stokes equation.; Panel method (Fluid dynamics).; Poisson equation.; Rectangular wings.; Steady flow.; Three dimensional flow.; Transonic flow.; Unsteady flow.; Wing panels.
Other titles: Steady and unsteady three dimensional transonic ...
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0063-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 2 microfiches.