NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Validation of a High-Order Compact Code for Nonlinear Flows About Complex GeometricThe slides review computational requirements for nozzle exhaust flow and noise calculations and the current numerical method, validation of prefactored compact scheme on CAA benchmark problems, a curvilinear grid performance test of gust response of a Joukowski airfoil, airfoil surface RMS pressure distribution and far field noise radiation results for Joukowski airfoil in a vortical gust, boundary distance study for Joukowski airfoil problem, and performance of ICOMP parallel Macintosh cluster.
Document ID
20040201019
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Hixon, Ray (NASA Glenn Research Center Cleveland, OH, United States)
Mankbadi, R. R. (Embry-Riddle Aeronautical Univ.)
Date Acquired
September 7, 2013
Publication Date
November 1, 2001
Publication Information
Publication: Proceedings of the Jet Noise Workshop
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle20040200997Collected WorksProceedings of the Jet Noise Workshop
No Preview Available