Simulations of the Flow in Supersonic Turbines with Straight Centerline Nozzles
Author:
Affiliation:
1. Virginia Commonwealth University, Richmond, Virginia 23284-3015
2. NASA Marshall Space Flight Center, Huntsville, Alabama 35812
3. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5580
Reference5 articles.
1. Application of an unsteady Navier-Stokes solver to transonic turbinedesign
2. Approximate Riemann solvers, parameter vectors, and difference schemes
3. Unsteady analysis of hot streak migration in a turbine stage
4. Highly parallel computers: Perspectives
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