Design and characterization of a multifunctional low-speed anechoic wind tunnel at HKUST: Aerospace Science and Technology

Keyphrases

• University of Hong Kong 100%
• Low Speed 100%
• Wind Tunnel 100%
• Aerodynamic Performance 100%
• Aerospace Technology 100%
• Trailing Edge Noise 100%
• Anechoic Wind Tunnel 100%
• Aeroacoustic Performance 100%
• Aerospace Science 100%
• Hong Kong 50%
• Design Principles 50%
• Measurement System 50%
• Flat Plate 50%
• Power-law Scaling 50%
• Silencer 50%
• Design Requirements 50%
• Flow Speed 50%
• Closed Circuit 50%
• Low Background Noise 50%
• Anechoic Chamber 50%
• Axial Fan 50%
• Tunnel Section 50%
• Injection Test 50%
• Evaluation Device 50%
• Jet Test 50%
• Contraction Section 50%
• Fifth Powers 50%
• Closed Test Section 50%
• Low Noise 50%
• Noise Injection 50%

Engineering

• Aerospace Engineering 100%
• Tunnel 100%
• Test Section 50%
• Trailing Edge 50%
• Aerodynamics 50%
• Measurement System 25%
• Good Performance 25%
• Flow Speed 25%
• Scaling Law 25%
• Design Constraint 25%
• Closed Circuit 25%
• Exit Plane 25%
• Anechoic Chamber 25%
• Device Evaluation 25%
• Metrics 25%
• Open-Jet Test Section 25%
• Closed Test Section 25%
• Flat Plate 25%

Physics

• Wind Tunnels 100%
• Aeroacoustics 50%
• Aerodynamics 50%
• Flat Plate 25%
• Low Noise 25%