Actions for Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-wing Fighter-bomber-type Airplane with a Top Inlet at Mach Numbers from 1.6 to 2.35.

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Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-wing Fighter-bomber-type Airplane with a Top Inlet at Mach Numbers from 1.6 to 2.35.

Author
Gnos, A Vernon
Published
March 3, 1958.
Physical Description
1 electronic document
Additional Creators
Kurkowski, Richard L
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: 19930090135.
Accession ID: 93R19425.
NACA-RM-A57K20.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15427924