共 50 条
- [2] Effect of stagnation temperature on the supersonic axisymmetric minimum length nozzle conception with application for air Thermophysics and Aeromechanics, 2010, 17
- [5] Supersonic Dual Bell Axisymmetric Minimum Length Nozzle Conception for High Propulsion Thrust International Journal of Aeronautical and Space Sciences, 2019, 20 : 673 - 687
- [6] Supersonic two-dimensional minimum length nozzle design at high temperature. Application for air Chinese Journal of Aeronautics, 2007, 20 (01): : 29 - 39
- [9] Stagnation Temperature Effect on the Flow in the Supersonic Axisymmetric Minimum Length Nozzlewith Application for Air JOURNAL OF THE CHINESE SOCIETY OF MECHANICAL ENGINEERS, 2019, 40 (06): : 741 - 751
- [10] Stagnation Temperature Effect on the Flow in the Supersonic Axisymmetric Minimum Length Nozzlewith Application for Air Journal of the Chinese Society of Mechanical Engineers, Transactions of the Chinese Institute of Engineers, Series C/Chung-Kuo Chi Hsueh Kung Ch'eng Hsuebo Pao, 2019, 40 (06): : 741 - 751