From the time that wind tunnel wall interference was recognized to be significant, researchers have been developing methods to alleviate or account for it. Despite the best effort so far, it appears that no method is available which completely eliminates the effects due to the wind tunnel walls. This report discusses procedures developed for slotted wall and adaptive wall test sections of the Langley 0.3-m Transonic Cryogenic Tunnel (TCT) to assess and correct for the residual interference by methods consistent with the transonic nature of the tests.
Nonlinear Transonic Wall-Interference Assessment/Correction (WIAC) Procedures and Application to CAST-10 Airfoil Results from the NASA 0.3-M TCT 8- by 24-Inch Slotted Wall Test Section (SWTS)
1989
27 pages
Report
Keine Angabe
Englisch
Aerodynamics , Test Facilities & Equipment , Laboratory & Test Facility Design & Operation , Fluid Mechanics , Aerodynamic interference , Airfoils , Flow distribution , Transonic flow , Wall flow , Wind tunnel tests , Wind tunnel walls , Applications programs (Computers) , Correction , Cryogenic wind tunnels , Drag , Lift , Nonlinearity , Transonic wind tunnels