NASA Environmentally Responsible Aviation Hybrid Wing Body Flow-Through Nacelle Wind Tunnel CFD

• Published in: NASA Center for AeroSpace Information (CASI). Conference Proceedings
• Main Authors: Schuh, Michael J, Garcia, Jospeh A, Carter, Melissa B, Deere, Karen A, Stremel, Paul M, Tompkins, Daniel M
• Format: Conference Proceeding
• Language: English
• Published: Hampton NASA/Langley Research Center 04.01.2016
• Subjects: Aerospace industry; Aircraft industry; Aviation; Computational fluid dynamics; Computer simulation; Configurations; Low speed wind tunnels; Mathematical models; Nacelles; Scale models; Simulation; Wind tunnel testing; Wind tunnels

Wind tunnel tests of a 5.75% scale model of the Boeing Hybrid Wing Body (HWB) configuration were conducted in the NASA Langley Research Center (LaRC) 14'x22' and NASA Ames Research Center (ARC) 40'x80' low speed wind tunnels as part of the NASA Environmentally Responsible Aviatio...