Optimizing a Boundary-Layer-Ingestion Offset Inlet by Discrete Adjoint Approach
Author:
Affiliation:
1. NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
2. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050222
Reference28 articles.
1. Designing and Testing a Blended Wing Body with Boundary-Layer Ingestion Nacelles
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