1. Cumpsty NA (1989) Compressor aerodynamics. Longman Scientific & Technical, U.K
2. Moses JJ, Kazberovisch TI (1948) Effect of size and number of outlet pipes on design of collectors for rating and testing axial flow compressors. In: NACA technical note no.1607, Flight Propulsion Research laboratory Cleveland, Ohio. Sannders AJ, Hassan KK, Rabe DC (2004) Experimental and numerical study of stall flutter in a transonic low aspect ratio fan blisk. In: ASME
3. Senoo Y, Kawaguchi N (1983) Pressure recovery of collectors with annular curved diffusers. The American Society of Mechanical Engineers. ASME Paper No. 83-GT-35. Chiang HD, Keilb RE (1993) An analysis system for blade forced response. ASME J Turbomachinery 115(4):762–770
4. Xingsu L, Kunyuan P, Zuomin W (1981) Aerodynamic design and experimental study of marine gas turbine exhaust volutes. The American Society of Mechanical Engineers. ASME Paper No. 81-GT-143. Vahdati M, Simpson G, Imregun M (2009) Mechanisms for wide chord fan blade flutter. In: ASME Turbo Expo 2009, GT 2009-60098
5. Pradeep AM, Roy B, Vaibhav V, Srinuvasu D (2010) Study of gas turbine exhaust diffuser performance and its enhancement by shape modifications. In: Proceedings of ASME Turbo Expo 2010. ASME Paper No. GT2010-22088