Parameter Value Unit Weight (W) lbskg Air Density (ρ) slugs/ft³kg/m³ Wing Area (S) ft²m² Max Coefficient of Lift (CLmax) Calculate Stall Speed Result Value Unit Stall Speed m/s Stall Speed km/h Stall Speed ft/s Stall Speed mph Stall Speed knots
Explore our Aerodynamics section, featuring simple online calculators for various applications. WebXFOIL is an online application for XFOIL v6.99, a tool used for the design and analysis of subsonic isolated airfoils. Explore aerodynamic performance easily through your web browser.
up to 81 km altitude Altitude: metersfeet Delta T (K): Airspeed: m/skm/hmphknots Reference Length: metersfeet Select Unit System: Standard International Units (SI)English Units Calculate Results
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Within the field of computational fluid dynamics (CFD), NASA benchmarks hold significant importance as they serve as fundamental standards for validating simulation methods and software. These benchmarks are essential in ensuring the accuracy and reliability of open-source software used in aerospace and engineering applications. Here, you’ll find a variety of validation cases designed for different
