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Approximation of the spanwise distribution of wind-tunnel-boundary interference on lift of wings in rectangular perforated-wall test sections

Author:
Schilling, B. L.
Published:
May 1, 1968.
Physical Description:
1 electronic document
Additional Creators:
Wright, R. H.
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary:
Approximation method for calculating spanwise distribution of wind tunnel boundary interference on wing lift in rectangular perforated wall
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19680015145.
Accession ID: 68N24617.
NASA-TR-R-285.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15955265