Preliminary Performance Analysis of the LAPCAT-MR2 by means of Nose-to-Tail Computations
Author:
Affiliation:
1. ESA-ESTEC
2. CIRA, Centro Italiano Ricerche Aerospaziali
3. CIRA, Centro Italiano Ricerche Aerospaziali)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5872
Reference16 articles.
1. Detached-eddy simulation with compressibility corrections applied to a supersonic axisymmetric base flow
2. An Implicit Multigrid Method for Turbulent Combustion
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