Full Scale Tests of Wood Propellers on a VE-7 Airplane in the Propeller Research Tunnel (open access)

Full Scale Tests of Wood Propellers on a VE-7 Airplane in the Propeller Research Tunnel

"The investigation described in this report was made primarily to afford a comparison between propeller tests in the new propeller research tunnel and flight tests and small model tests on propellers. Three wood propellers which had been previously tested in flight on a VE-7 airplane, and of which models had also been tested in a wind tunnel, were tested again on a VE-7 airplane in the propeller research tunnel. The results of these tests are in fair agreement with those of the flight and model tests" (p. 445).
Date: June 18, 1928
Creator: Weick, Fred E.
System: The UNT Digital Library
Full Scale Tests on a Thin Metal Propeller at Various Tip Speeds (open access)

Full Scale Tests on a Thin Metal Propeller at Various Tip Speeds

"This report describes an investigation made in order to determine the effect of tip speed on the characteristics of a thin-bladed metal propeller. The propeller was mounted on a VE-7 airplane with a 180-HP E-2 engine, and tested in the 20-foot propeller research tunnel of the National Advisory Committee for Aeronautics. It was found that the effect of tip speed on the propulsive efficiency was negligible within the range of the tests, which was from 600 to 1,000 feet per second (about 0.5 to 0.9 the velocity of sound in air)" (p. 465).
Date: June 20, 1928
Creator: Weick, Fred E.
System: The UNT Digital Library
An Investigation of the Use of Discharge Valves and an Intake Control for Improving the Performance of N.A.C.A. Roots Type Supercharger (open access)

An Investigation of the Use of Discharge Valves and an Intake Control for Improving the Performance of N.A.C.A. Roots Type Supercharger

"This report presents the results of an analytical investigation on the practicability of using mechanically operated discharge valves in conjunction with a manually operated intake control for improving the performance of N. A. C. A. Roots type superchargers. These valves, which may be either of the oscillating or rotating type, are placed in the discharge opening of the supercharger and are so shaped and synchronized with the supercharger impellers that they do not open until the air has been compressed to the delivery pressure. The intake control limits the quantity of air compressed to engine requirements by permitting the excess air to escape from the compression chamber before compression begins" (p. 479).
Date: June 29, 1928
Creator: Schey, Oscar W. & Wilson, Ernest E.
System: The UNT Digital Library
Speed and deceleration trials of U.S.S. Los Angeles (open access)

Speed and deceleration trials of U.S.S. Los Angeles

From Summary: "The trials reported in this report were instigated by the Bureau of Aeronautics of the Navy Department for the purpose of determining accurately the speed and resistance of the U. S. S. "Los Angeles" with and without water recovery apparatus, and to clear up the apparent discrepancies between the speed attained in service and in the original trials in Germany. The trials proved very conclusively that the water recovery apparatus increases the resistance about 20 per cent, which is serious, and shows the importance of developing a type of recovery having less resistance. Between the American and the German speed trials without water recovery there remains an unexplained discrepancy of nearly 6 per cent in speed at a given rate of engine revolutions."
Date: June 12, 1928
Creator: De France, S. J. & Burgess, C. P.
System: The UNT Digital Library