Microphone Array Measurement in European Transonic Wind Tunnel at Flight Reynolds Numbers

AIAA Journal - United States
doi 10.2514/1.j055262
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Wind-Tunnel Tests of Two Airfoils for Wind Turbines Operating at High Reynolds Numbers

2000English

Variable-Pressure Wind Tunnel Test of Airfoils at Low Reynolds Numbers Designed for Mars Exploration Aircraft

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
2016English

Wind Loads on Heliostats and Photovoltaic Trackers at Various Reynolds Numbers

Journal of Wind Engineering and Industrial Aerodynamics
Mechanical EngineeringCivilRenewable EnergyStructural EngineeringSustainabilitythe Environment
2011English

Minimally Constrained Flight Simulation in Wind Tunnel

Journal of Aircraft
2019English

Numerical Study of Wall Ventilation in a Transonic Wind Tunnel

Journal of Aerospace Technology and Management
Aerospace Engineering
2015English

An Experimental Investigation of Fixed-Geometry Diffusers in an Open-Jet Wind Tunnel at Mach Numbers Between 14 and 18 and Reynolds Numbers Between 8,900 and 25,000

1967English

Aerodynamics of Flapping Wing at Low Reynolds Numbers: Force Measurement and Flow Visualization

ISRN Mechanical Engineering
2011English

Study of Asymptotic Theory of Transonic Wind Tunnel Wall Interference

1984English

Free-Flight Force Measurement Technique in Shock Tunnel

2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy