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Testing and analysis of dual-mode adaptive landing gear, taxi mode test system for YF-12A

Author
Gamon, M. A.
Published
Sep 1, 1979.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The effectiveness of a dual mode adaptive landing gear system in reducing the dynamic response of an airplane during ground taxiing was studied. The dynamic taxi tests of the YF-12A research airplane are presented. A digital computer program which simulated the test conditions is discussed. The dual mode system as tested provides dynamic taxi response reductions of 25 percent at the cg and 30 to 45 percent at the cockpit.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19790023021.
Accession ID: 79N31192.
NASA-CR-144884.
LR-28776.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15724703