Wind-Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-Opening Slot (1932)
NASA Technical Reports Server (NTRS) · leaf 7
6 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Figure 4.—Airfoil mounted in tunnel wing pressure on certain aerodynamic characteristics fies the average pressure inside the airfoil measured and in the» value of certain criteria. with respect to the static pressure of the tunnel test The hft and drag values were reduced to absolute section. For…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
![An illustration from The space-threshold of colours and its dependence upon contrast [microform] : first article (1898)](https://img.insideoutlibrary.com/img/200/ia-cihm_01297-29-0.webp)
