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The Maximum Delivery Pressure of Single-Stage Radial Superchargers for Aircraft Engines
With the aid of simple considerations and test results, an attempt is made to clear up some obscure points that still exist. The considerations are restricted to those cases where it is in fact of advantage to"force" the large delivery heads required for high altitude and high supercharge with a single-stage supercharger.
Date:
August 1940
Creator:
von der Nüll, W.
System:
The UNT Digital Library
A Simple Approximation Method for Obtaining the Spanwise Lift Distribution
The approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates.
Date:
August 1940
Creator:
Schrenk, O.
System:
The UNT Digital Library