Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)-Reference-Cited by-同舟云学术

Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
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Author:

Flamm Jeff D.¹,James Kevin²,Bonet John T.³

Affiliation:

1. NASA Langley Research Center

2. NASA Ames Research Center

3. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0007

Reference17 articles.

1. 1Bonet, J. T., Schellenger, H. G., Rawdon, B. K., Elmer, K. R., Wakayama, S. R., Brown, D. L., and Guo, Y. “Environmentally Responsible Aviation (ERA) Project - N+2 Advanced Vehicle Concepts Study and Conceptual design of Subscale Test Vehicle (STV) Final Report,” NASA/CR-2011-216519.

2. Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration

3. 3Bonet, J. T., Dickey, E., Princen, N., Sexton, M., Beyar, M., Tompkins, D. M., Kawai, R., Camacho, P., and Elmer, K. “Environmentally Responsible Aviation (ERA) Project ? Hybrid Wing Body Engine/Airframe Operability Testing Final Report,” NASA/CR-2015.

4. CFD Predictions for Transonic Performance of the ERA Hybrid Wing-Body Configuration (Invited)

5. Overview of Low-speed Aerodynamic Tests on a 5.75% Scale Blended-Wing-Body Twin Jet Configuration (Invited)

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