Use of Active Learning to Design Wind Tunnel Runs for Unsteady Cavity Pressure Measurements

林子辰（2020）。The Application of Pressure Sensitive Paints for Measurement of the Shock Waves in Microscale Supersonic Wind Tunnels〔碩士論文，國立清華大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0016-2502202114243680
高郡壎（2012）。Numerical Simulation and Wind Tunnel Experiment of Small Multi-Bladed Wind Turbines〔碩士論文，淡江大學〕。華藝線上圖書館。https://doi.org/10.6846/TKU.2012.00213
Wang, C. S. (1999). Review and Prospect of Numerical Wind Tunnel Development. 中國航空太空學會學刊, 31(4), 253-259. https://doi.org/10.6124/TAASRC.199912_31(4).01
王安邦、陳信賓（1995）。Low-Turbulence Closed-Return Wind-Tunnel: Model Design and Testing。中國航空太空學會學刊，27(4)，297-306。https://doi.org/10.6124/TAASRC.199512_27(4).03
王冠傑（2014）。Complex terrain of the comparisons between wind velocity and wind pressure in monitoring and wind tunnel test〔碩士論文，淡江大學〕。華藝線上圖書館。https://doi.org/10.6846/TKU.2014.00156