A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase-Reference-Cited by-同舟云学术

A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA Aviation Technology, Integration, and Operations Conference
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Author:

Chakraborty Imon¹,Trawick David R.¹,Mavris Dimitri N.¹,Emeneth Mathias²,Schneegans Alexander²

Affiliation:

1. Georgia Institute of Technology

2. PACE America, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3012

Reference58 articles.

1. Aircraft Engine Design, Second Edition

2. The all-electric aircraft

3. The more electric aircraft—assessing the benefits

4. 5National Transportation Safety Board (NTSB), "Aircraft Accident Report - United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July19,1989," Tech. Rep. NTSB/AAR-90/06, 1990.

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