Flow Simulation of N2B Hybrid Wing Body Configuration

Author:

Kim Hyoungjin1,Liou Meng-Sing2

Affiliation:

1. ASRC Aerospace Corporation

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. 1NASA Research and Technology Program and Project Management Requirements, NASA Procedural Requirements7120.9.AppendixJ.TechnologyReadinessLevels(TRLs),February05,2008.

2. Design of the Blended Wing Body Subsonic Transport

3. 3Kawai, R. and Brown, D. "Acoustic Prediction Methodology and Test Validation for an Efficient Low-Noise Hybrid Wing Body Subsonic Transport," Phase I Final Report PWDM08-006A, NASA Contract Number NNL07AA54C,October,2008.

4. 5delaRosaBlanca,E.,Hall,C.A.,andCrichton,D."ChallengesintheSilentAircraftEngineDesign,"AIAAPaper 2007-454,Jan.,2007.

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