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Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers
From Summary: "Wind-tunnel tests of a full-scale two-blade NACA 10-(10)(08)-03 (high camber) propeller have been made for a range of blade angles from 20 degrees to 55 degrees at airspeeds up to 500 miles per hour. The results of these tests have been compared with results from previous tests of the NACA 10-(3) (08)-03 (low camber) and NACA 10-(5)(08)-03 (medium camber) propellers to evaluate the effects of blade-section camber on propeller aerodynamic characteristics."
Date:
May 6, 1948
Creator:
Maynard, Julian D. & Salters, Leland B., Jr.
System:
The UNT Digital Library
Flutter Investigation in the Transonic Range of Six Airfoils Attached to Three Freely Falling Bodies
Report presenting testing of six flutter wings, two swept 45 degrees and four unswept, attached to three freely falling bodies. Flutter frequency and phasing were recorded.
Date:
May 6, 1948
Creator:
Clevenson, S. A. & Lauten, William T., Jr.
System:
The UNT Digital Library