Sensitivity of Mission Energy Consumption to Turboelectric Distributed Propulsion Design Assumptions on the N3-X Hybrid Wing Body Aircraft-Reference-Cited by-同舟云学术

Sensitivity of Mission Energy Consumption to Turboelectric Distributed Propulsion Design Assumptions on the N3-X Hybrid Wing Body Aircraft

Published:2012-07-30 Issue: Volume: Page:
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Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Felder James,Tong Michael,Chu Julio

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. 1Del Rosario, R., Follen, G., Wahls, R. Madavan, N, "Subsonic Fixed Wing Project Overview and Technical Challenges for Energy Efficient Environmentally Compatible Subsonic Transport Aircraft", 50th AIAA Aerospace Science Meeting, Nashville, TN, 9-12Jan. 2012

2. 2Felder,J.,Brown,G.,Kim,H.,Chu,J."TurboelectricDistributedPropulsioninaHybridWingBodyAircraft",20thISABEConference, Götenberg, Sweden, 12-16Sept.,2011

3. 9Grady, J, "Overview of CMC Research at the NASA Glenn Research Center", 35thAnnual Conference on Composites, Materials and Structures",24-27Jan., 2011

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