X353-5B AND X376 DESIGN SUMMARY REPORT
GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT
Pagination or Media Count:
Installation studies for compatibility of the X353-5B and X376 propulsion systems to the XV-5A aircraft are described as well as the aerodynamic mechanical design aspects of he lift fan system. Discussions are centered around the changes to the fans developed beyond contract DA 44-177-TC- 584.
- Research and Experimental Aircraft