An assessment of intake efficiency has been performed through calculations to obtain scramjet propulsive performance (specific impulse, ... The significant findings of this study are as f ol lows . the ideal isentropic inlet is about 3aquot;/. throughout the hypersonic Mach number range. ... John, James E. GAS DYNAMICS. , Allyn and Bacon Inc., Boston, 1969. ... Oussama Rizkalla, Wallace Chinitz, John I. Erdos.
|Title||:||ICAS proceedings, 1990|
|Author||:||International Council of the Aeronautical Sciences. Congress, American Institute of Aeronautics and Astronautics, International Council of the Aeronautical Sciences|