1. Cousins, W.T. 2004. History, philosophy, physics, and future directions of aircraft propulsion system/inlet integration. In ASME Turbo Expo 2004: power for land, sea and air, Vienna, Austria, 14-17 June 2004.
2. Bobbala, G.A. 1979. Effect of steady-state pressu\re distortion on stall margin of a J85-21 turbine engine. NASA-TM-79123 E-9958 NASA Lewis research center.
3. Calogeras, J.E., and C.M. Mebalic. 1971. Experimental investigation of the effect of screen-induced total-pressure distortion on turbojet stall margin, NASA TMX-2239 March.
4. Gas Turbine inlet flow distortion guidelines. Aerospace Recommended practice 1420. Society of automotive engineers.
5. Inter total-pressure-distortion considerations for gas turbine engines. Aerospace information report 1419. AIR 1419.