Affiliation:
1. Queen's University Belfast
Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Saving costs in design, manufacturing and operation of aero engine parts
2. Reverser Concepts for Subsonic Transport Applications",NASA/TM-2000-210300, 1. For the limiting value of vane displacement of 0.4mm, a minimum of two transverse supports are required. This results in a 1.6%weightsaving ina singlecascadebox.
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2 articles.
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