Actions for Longitudinal aerodynamic parameters of the Kestrel aircraft (XV-6A) extracted from flight data

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Longitudinal aerodynamic parameters of the Kestrel aircraft (XV-6A) extracted from flight data

Author
Williams, J. L.
Published
Jun 1, 1973.
Physical Description
1 electronic document
Additional Creators
Suit, W. T.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Flight-test data have been used to extract the longitudinal aerodynamic parameters of a vectored-thrust aircraft. The results show that deflecting the thrust past 15 has an effect on the pitching-moment derivatives and tends to reduce the static stability. The trend toward reduction in the longitudinal stability also been noted by the pilots conducting the flight tests.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19730015339.
Accession ID: 73N24066.
NASA-TN-D-7296.
L-8703.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15749168