6Saravanmuttoo H I H . Recommended practice for meas urement of gas path pressures and temperatures for performance assesment of air- craft turbine engines and components. AGARD Advisory Report No. 245, 1990.
7Bui T T, Oates D L. Design and evaluation of a new boundary-layer measurement rake for flight testing. NASA TM-2000-209014,2000.
8Quinn R D, Gong L. In-fllght boundary-layer measurements on a hol- low cylinder at Mach number of 3. 0. NASA TP-1980-1764.
9Aulehla F. Intake swir a major disturbance parameter in engine/intake compatibility. 13th Congress of ICAS/AIAA, Seattle,1982.
10Guo R W, Seddon J. The swirl in a s-duct of typical air intake propor- tions. The Aeronautical Quarterly, 1982.
