Actions for Free-flight Measurements at Mach Numbers from 0.7 to 1.6 of Some Effects of Airfoil-thickness Distribution and Trailing-edge Angle on Aileron Rolling Effectiveness and Drag for Wings with 0 and 45 Degrees Sweepback

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Free-flight Measurements at Mach Numbers from 0.7 to 1.6 of Some Effects of Airfoil-thickness Distribution and Trailing-edge Angle on Aileron Rolling Effectiveness and Drag for Wings with 0 and 45 Degrees Sweepback

Author
Strass, H Kurt
Published
October 08, 1951.
Physical Description
1 electronic document
Additional Creators
Fields, E M
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930086680.
Accession ID: 93R15970.
NACA-RM-L51G27.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15431406