Strip distortion generator for simulating inlet flow distortion in gas turbine engine ground test facilities

Author:

Saleem Yusoof M.,Sivapragasam M.,Deshpande M.D.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference29 articles.

1. J.P. Longley, E.M. Greitzer, Inlet distortion effects in aircraft propulsion system integration, in: Proceedings of Steady and Transient Performance Prediction of Gas Turbine Engines, AGARD-LS-183, pp. 6-1–6-18, 1992.

2. M. Sivapragasam, S. Ramamurthy, Inlet Flow Distortion Effects in Aircraft Gas Turbine Engine Compression Systems, National Aerospace Laboratories, Bangalore, NAL TM PR 0901, 2009.

3. D.K. Beale, K.B. Cramer, P.S. King, Development of Improved Methods for Simulating Aircraft Inlet Distortion in Turbine Engine Ground Tests, AIAA Paper No. 2002–3045, 2002.

4. B.W. Overall, A Procedure for the Design of Complex Distortion Screen Patterns for Producing Specified Steady-state Total Pressure Profiles at the Inlet of Turbine Engines, Arnold Engineering Development Center, Tennessee, AEDC-TR-72-10, 1972.

5. R.E. Anderson, Aircraft Engine Inlet Pressure Distortion Testing in a Ground Test Facility, AIAA Paper No. 83-1233, 1983.

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