Guía completa de termodinámica, transferencia de calor & y masa e ingeniería de líquidos
Español English Русский 中文 Português Français Deutsch Acerca de Junta editorial Contacto Acceso Begell House

Visualization of the boundary layer transition in low-speed flow

This movie presents a full set of images from a wind tunnel test combined in an animation. In the test, the 65° delta wing model of 420 mm length and 332 mm span was tested in subsonic wind tunnel at constant flow speed of 50 m/s and varying the angle of attack

Read more in Visualization of boundary layer transition by viscous oil

Volver arriba © Copyright 2010-2022
Índice A-Z Autor / Editores Mapa Semántico Galería Visual Contribuir Guest