Actions for A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6.

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A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6.

Author
Hoffman, Sherwood
Physical Description
1 electronic document
Online Version

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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: 19930088324.
Accession ID: 93R17614.
NACA-RM-L54H13a.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15430160