Gortler instability and supersonic quiet nozzle design
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. High Technology Corporation, Hampton, Virginia 23666
3. George Washington University, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11184
Reference5 articles.
1. Boundary-layer transition on a cone and flat plate at Mach 3.5
2. Advanced Mach 3.5 Axisymmetric Quiet Nozzle
3. Free stream noise and transition measurements in a Mach 3.5 pilot quiet tunnel
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