NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Stability analysis for laminar flow control, part 1The basic equations for the stability analysis of flow over three dimensional swept wings are developed and numerical methods for their solution are surveyed. The equations for nonlinear stability analysis of three dimensional disturbances in compressible, three dimensional, nonparallel flows are given. Efficient and accurate numerical methods for the solution of the equations of stability theory were surveyed and analyzed.
Document ID
19780004420
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Benney, D. J. (Cambridge Hydrodynamics, Inc. Cambridge, MA, United States)
Orszag, S. A. (Cambridge Hydrodynamics, Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-2910
CHI-2
Report Number: NASA-CR-2910
Report Number: CHI-2
Accession Number
78N12363
Funding Number(s)
CONTRACT_GRANT: NAS1-14427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available