Actions for An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.59.

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An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.59.

Author
Spearman, M Leroy
Published
May 23, 1950.
Physical Description
1 electronic document
Additional Creators
Cooper, Morton
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: 19930086319.
Accession ID: 93R15609.
NACA-RM-L50C24.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15431694