1. Reid, L., Moore, R.D.: Design and overall performance of four highly loaded, high-speed inlet stages for an advanced high-pressure-ratio core compressor. NASA TP 1337 (1978)
2. ASME Turbomachinery Committee, CFD Code Assessment in Turbomachinery - Author’s Information Package (June 1993)
3. Shabbir, A., Celestina, M.L., Adamczyk, J.J., Strazisar, A.J.: The effect of hub leakage on two high speed axial flow compressor rotors. ASME Paper 97-GT-346 (1997)
4. AGARD Advisory Report 355, CFD Validation for Propulsion System Components, Report of the Propulsion and Energetics Panel Working Group 26 (1998)
5. Home page of the European FP5 research project JEAN (Jet Exhaust Aerodynamics and Noise),
http://www.ist-world.org/ProjectDetails.aspx?ProjectId=14e67d914b3141cabcf1b1499e404a0a