共 50 条
- [41] Prediction of rotor blade vortex interaction noise using 3-D unsteady surface pressure Hangkong Xuebao, 6 (723-727):
- [42] Numerical prediction of vortex trajectories and vortex-blade interaction on the CROR engine AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2020, 92 (09): : 1345 - 1356
- [43] Sensitivity of helicopter blade-vortex-interaction noise and vibration to interaction parameters JOURNAL OF AIRCRAFT, 2005, 42 (03): : 685 - 697
- [44] Feedback attenuation and adaptive cancellation of blade vortex interaction noise on a helicopter blade element PROCEEDINGS OF THE 1998 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 1998, : 1053 - 1057
- [45] EFFECT OF TIP VORTEX STRUCTURE ON HELICOPTER NOISE DUE TO BLADE-VORTEX INTERACTION JOURNAL OF AIRCRAFT, 1980, 17 (10): : 705 - 711
- [47] High-precision prediction on unsteady aeroelastic loads of helicopter rotors under blade-vortex interaction condition Hangkong Dongli Xuebao/Journal of Aerospace Power, 2015, 30 (05): : 1267 - 1274
- [48] Numerical prediction of aerodynamic loads acting on a blade section-model oscillating in stall SCIENCE OF MAKING TORQUE FROM WIND, TORQUE 2024, 2024, 2767