Bookmark

Report an Issue

Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds

Author: Matranga, Gene J
Physical Description: 1 electronic document
Additional Creators: Armistead, Katharine H

Online Version

hdl.handle.net , Connect to this object online.

Availability

Finding items...

Restrictions on Access: Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Collection: NASA Technical Reports Server (NTRS) Collection.
Note: Document ID: 19930089937.
Accession ID: 93R19227.
NACA-RM-H58A03a.
Terms of Use and Reproduction: No Copyright.

View MARC record | catkey: 15428795