The response of normal shocks in diffusers

Author:

Sajben Miklos1

Affiliation:

1. McDonnell Douglas Research Laboratories, St. Louis, Missouri

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference9 articles.

1. Using a global hydrogen-air combustion model in turbulent reacting flow calculations

2. Derivation and significance of second-order modal design sensitivities

3. Rayleigh, Lord, The Theory of Sound, Vol.I, Dover, New York, 1945, pp.113-118, 136-137.

4. 3Courant, R. and Hilbert, D., Methods of Mathematical Physics, Vol.I, Interscience, New York, 1953, pp.41-45, 343-350.

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1. Overview of Flow Oscillations in Transonic and Supersonic Nozzles;Journal of Propulsion and Power;2006-07

2. Theoretical Prediction of Resonance in Nozzle Flows;Journal of Propulsion and Power;2005-03

3. Simulation of Unsteady Three Dimensional Separation Behaviour in Truncated Ideal Contour Nozzles;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

4. A Brief Overview on some Resonance Phenomena in Nozzle Flows;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

5. Self-excited oscillations in internal transonic flows;Progress in Aerospace Sciences;1990-01

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