Qin et al., 2022 - Google Patents
Numerical simulation of hydrodynamic and noise characteristics for a blended-wing-body underwater gliderQin et al., 2022
- Document ID
- 6369190606653534595
- Author
- Qin D
- Huang Q
- Pan G
- Shi Y
- Li F
- Han P
- Publication year
- Publication venue
- Ocean Engineering
External Links
Snippet
The present study compares the hydrodynamic and noise characteristics of a second- generation underwater glider, ie, the blended-wing-body glider, and a traditional Slocum glider, based on large eddy simulation and Ffowcs–Williams and Hawkings equation …
- 238000004088 simulation 0 title abstract description 23
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/10—Measures concerning design or construction of watercraft hulls
- Y02T70/12—Improving hydrodynamics of hull
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
- Y02T50/16—Drag reduction by influencing airflow
- Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Zhang et al. | Aerodynamic control of low-Reynolds-number airfoil with leading-edge protuberances | |
Jones et al. | Experimental and computational investigation of the Knoller-Betz effect | |
Qin et al. | Numerical simulation of hydrodynamic and noise characteristics for a blended-wing-body underwater glider | |
Li et al. | Aerodynamic prediction of iced airfoils based on modified three-equation turbulence model | |
Guo et al. | Influence of jet flow on the hydrodynamic and noise performance of propeller | |
Khalid et al. | Quantification of flow noise produced by an oscillating hydrofoil | |
Liu et al. | Numerical investigation of unsteady vortex breakdown past 80/65 double-delta wing | |
Siozos-Rousoulis et al. | A flow control technique for noise reduction of a rod-airfoil configuration | |
Hristov et al. | Poststall hysteresis and flowfield unsteadiness on a NACA 0012 airfoil | |
Wang et al. | Numerical research on the influence of sail leading edge shapes on the hydrodynamic noise of a submarine | |
Ganesan et al. | Computational fluid dynamic analysis of an unmanned amphibious aerial vehicle for drag reduction | |
Kamliya Jawahar et al. | Aerodynamic and Aeroacoustic Performance of Three-element High Lift Airfoil fitted with Morphing Fillers | |
Zhang et al. | Flow and noise characteristics of blunt-trailing-edge flat plate with an upstream cylinder | |
Xu et al. | Delayed detached eddy simulations of fighter aircraft at high angle of attack | |
Wani et al. | Design & analysis of NACA 0012 airfoil with circular dent of 30 mm depth on upper surface | |
Lai et al. | Aeroacoustic investigation of multi-directional wings aligned in tandem under wing-in-ground effect | |
Lu et al. | Numerical investigation of the unsteady coupling airflow impact of a full-scale warship with a helicopter during shipboard landing | |
Li et al. | Large-Eddy Simulation of Low-Reynolds-Number Flow Around Partially Porous Airfoils | |
Deng et al. | Large Eddy Simulation and Noise Prediction of a Supercritical Airfoil at Moderate Angle of Attack | |
Imamura et al. | Noise simulation around NACA0012 wingtip using large eddy simulation | |
Li et al. | Airfoil noise reduction using boundary layer control | |
Yamamoto et al. | Progress on experimental and numerical research for slat noise in JAXA | |
Imamura et al. | Numerical simulation of NACA0012 wingtip flow leading to noise generation | |
Abdol-Hamid et al. | DPW-6 Results Using FUN3D With Focus on k-kL-MEAH2015 Turbulence Model | |
YashodharaRao et al. | Dynamics of fluid flow around aerofoil, and submarine: effect of winglets |