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Wind Tunnel and Propulsion Test Facilities29,99 €![Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface]( "Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface")
Wind-tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface20,99 €![Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests]( "Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests")
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Wind Tunnel Tests on a Low-wing Monoplane With Propeller Running20,99 €![Wind-tunnel Investigation of a Rectangular NACA 2212 Airfoil With Semispan Ailerons and With Nonperforated, Balanced Double Split Flaps for Use as Aerodynamic Brakes]( "Wind-tunnel Investigation of a Rectangular NACA 2212 Airfoil With Semispan Ailerons and With Nonperforated, Balanced Double Split Flaps for Use as Aerodynamic Brakes")
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Comparison of Wind-tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas A-26 Airplane18,99 €![Some Notes on the Determination of the Stick-free Neutral Point From Wind-tunnel Data]( "Some Notes on the Determination of the Stick-free Neutral Point From Wind-tunnel Data")
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Wind tunnel techniques involve experimental methods to study the aerodynamic characteristics of objects by simulating airflow in a controlled environment. A wind tunnel is a specialised facility where air is directed at varying speeds over scaled models or actual components of vehicles, buildings, or other structures. These techniques analyse lift, drag, pressure distribution, flow visualisation, and aerodynamic stability. Various types of tunnels, such as subsonic, transoceanic, supersonic, and hyper sonic, cater to different speed regimes. Tools like smoke trails, pressure sensors, and force balances provide data for refining designs, optimising performance, and validating computational models in aerospace, automotive, and architectural applications.