An outflow boundary condition for aeroacoustic computations
By: M. Ehtesham Hayder, Thomas Hagstrom.
Contributors: Hagstrom, Thomas.; Lewis Research Center. Institute for Computational Mechanics in Propulsion.
Series: NASA technical memorandum -- 106930.
Publisher: National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion; National Technical Information Service, distributor
Published: 1995
Place of publication: Cleveland, Ohio; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroacoustics.; Axisymmetric flow.; Boundary conditions.; Computation.; Jet flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0744-M.

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