Assessment of Mach Number Correction for Sidewall Interference in Transonic Airfoil Testing
FLUID DYNAMICS - Test Time Increase by Delaying Driver Gas Contamination for Reflected Shock Tunnels
Gasdynamical Detectors of Driver Gas Contamination in a High-Enthalpy Shock Tunnel
Flow Visualization Studies on Sidewall Effects in Two-Dimensional Transonic Airfoil Testing
Detection of Driver Gas Contamination in the T5 Hypervelocity Shock Tunnel
Flow Angularity Measurement of JAXA 2m x 2m Transonic Wind Tunnel
Numerical Simulation of Flowfields of the NAL Two-Dimensional Transonic Wind Tunnel
Wall and Support Interference Corrections of NASA Common Research Model Wind Tunnel Tests in JAXA
Cell Structure on Circular Cylinders near the Critical Reynolds Number
Analysis of NASA Common Research Model Dynamic Data in JAXA Wind Tunnel Tests
Calibration of the Test Section Mach Number in the JAXA 2m x 2m Transonic Wind Tunnel
80% Scaled NASA Common Research Model Wind Tunnel Test of JAXA at Relatively Low Reynolds Number
Three-Dimensional Effects on Shock Wave Reflections in Steady Flows
Numerical Simulation of Flowfields of the NAL Two-Dimensional Transonic Wind Tunnel