Actions for Wind-tunnel Investigation of the Low-speed Static and Rotary Stability Derivatives of a 0.13-scale Model of the Douglas D-558-II Airplane in the Landing Configuration

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Wind-tunnel Investigation of the Low-speed Static and Rotary Stability Derivatives of a 0.13-scale Model of the Douglas D-558-II Airplane in the Landing Configuration

Author
Wells, Evalyn G
Published
August 27, 1952.
Physical Description
1 electronic document
Additional Creators
Queijo, M J
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: 19930087305.
Accession ID: 93R16595.
NACA-RM-L52G07.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15427140