An LU implicity scheme for high speed inlet analysis

An LU implicity scheme for high speed inlet analysis [microform] / Seokkwan Yoon and Antony Jameson ; [performing organization: Sverdrup Technology, Inc., Lewis Research Center and Princeton University ; sponsoring agency: National Aeronautics and Space Administration]

A numerical method is developed to analyze the inviscid flowfield of a high speed inlet by the solution of the Euler equations. The Lower-Upper Implicit scheme in conjunction with adaptive dissipation proves to be an efficient and robust nonoscillatory shock capturing technique for high Mach number...

Full description

Saved in:
Bibliographic Details
Main Author: Yoon, Seokkwan
Corporate Authors: Sverdrup Technology, Inc, Lewis Research Center, Princeton University, United States. National Aeronautics and Space Administration
Other Authors: Jameson, Antony, 1934-
Format: Government Document Microfilm Book
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1986.
Series:NASA contractor report ; NASA CR-175098.
AIAA paper ; no. 86-1520.
Subjects:
Computational fluid dynamics.
Inviscid flow > Mathematical models.
Jets > Fluid dynamics.
Fluid dynamics > Mathematical models.
Navier-Stokes equations.
Inlet flow.
Transonic flow.
Euler equations of motion.
Finite volume method.
Flow distribution.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.26:175098
NAS 1.26:175098 Restricted Place a Hold

Similar Items