NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Personal computer study of finite-difference methods for the transonic small disturbance equationCalculation of unsteady flow phenomena requires careful attention to the numerical treatment to the governing partial differential equations. The personal computer provides a convenient and useful tool for the development of meshes, algorithms, and boundary conditions needed to provide time accurate solution of these equations. The one-dimensional equation considered provides a suitable model for the study of wave propagation in the equations of transonic small disturbance potential flow. Numerical results for effects of mesh size, extent, and stretching, time step size, and choice of far-field boundary conditions are presented. Analysis of the discretized model problem supports these numerical results. Guidelines for suitable mesh and time step choices are given.
Document ID
19900059812
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bland, Samuel R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aerodynamics
Meeting Information
Meeting: International Congress of Fluid Mechanics
Location: Cairo
Country: Egypt
Start Date: January 2, 1990
End Date: January 4, 1990
Sponsors: Mansoura Univ., Cairo Univ., Virginia Polytechnic Inst. and State Univ.
Accession Number
90A46867
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available