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
Attachment-line flow on an infinite swept wingA proposed method for calculating three-dimensional incompressible laminar and turbulent boundary layers is investigated with respect to its applicability to incompressible attachment line flow on an infinite swept wing. The calculation results obtained exhibit satisfactory agreement with experimental data.
Document ID
19740037543
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cebeci, T. (Douglas Aircraft Co. Long Beach, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
February 1, 1974
Publication Information
Publication: AIAA Journal
Volume: 12
Subject Category
Aerodynamics
Accession Number
74A20293
Funding Number(s)
CONTRACT_GRANT: NAS1-11623
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

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