LOW SPEED WIND TUNNEL TESTS OF SEVERAL AIRFOIL SECTIONS THROUGH 360 ANGLE OF ATTACK
Author(s) -
James Reed
Publication year - 1954
Publication title -
osti oai (u.s. department of energy office of scientific and technical information)
Language(s) - English
Resource type - Reports
DOI - 10.2172/4351474
Subject(s) - airfoil , naca airfoil , wind tunnel , angle of attack , section (typography) , physics , subsonic and transonic wind tunnel , code (set theory) , materials science , aerospace engineering , mechanics , engineering , computer science , aerodynamics , turbulence , reynolds number , transonic , operating system , set (abstract data type) , programming language
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