Flutter Analysis of Supersonic Axial Flow Cascades Using A High Resolution Euler Solver

Flutter Analysis of Supersonic Axial Flow Cascades Using A High Resolution Euler Solver

Part 1, Formulation and Validation

Microform - 1992
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Publisher: Washington, DC : National Aeronautics and Space Administration, [1992]
Characteristics: 1 v
Additional Contributors: Reddy, T. S. R.
United States

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