共 50 条
- [1] SOME EFFECTS OF APPLYING SONIC-BOOM MINIMIZATION TO SUPERSONIC CRUISE AIRCRAFT DESIGN JOURNAL OF AIRCRAFT, 1980, 17 (03): : 182 - 186
- [2] An active control method for reducing sonic boom of supersonic aircraft Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2021, 39 (03): : 566 - 575
- [3] Preliminary Optimization of the Sonic Boom Properties for Civil Supersonic Aircraft JOURNAL OF AIRCRAFT, 2013, 50 (04): : 1295 - 1299
- [5] LOW SONIC-BOOM SUPERSONIC TRANSPORT THROUGH AIRCRAFT DESIGN ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1976, 24 (01): : 34 - 38
- [6] Limitations of flight regime of a supersonic transport aircraft (SST) by sonic boom 1976, 24 (02): : 82 - 89
- [8] Two supersonic business aircraft conceptual designs, with and without sonic boom constraint JOURNAL OF AIRCRAFT, 2005, 42 (03): : 775 - 786
- [9] Reduction of the sonic boom level in supersonic aircraft flight by the method of surface cooling Thermophysics and Aeromechanics, 2013, 20 : 669 - 678
- [10] Influence of the Configuration Elements of a Model of a Supersonic Passenger Aircraft on the Parameters of Sonic Boom Volkov, V.F. (volkov@itam.nsc.ru), 1600, Springer Science and Business Media, LLC (90): : 449 - 460