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From Summary: "A series of publications on the source-distribution methods for evaluating the aerodynamics of thin wings at supersonic speeds is summarized, extended, and unified. Included in the first part are the deviations of: (a) the linearized partial-differential equation for unsteady flow at a substantially constant Mach number. b) The source-distribution solution for the perturbation-velocity potential that satisfies the boundary conditions of tangential flow at the surface and in the plane of the wing; and (c) the integral equation for determining the strength and the location of sources to describe the interaction effects (as represented by upwash) of the bottom and top wing surfaces through the region between the finite wing boundary and the foremost Mach wave. The second part deals with steady-state thin-wing problems. The third part of the report approximates the integral equation for unsteady upwash and includes a solution of approximate equation. Expressions are then derived to evaluate the load distributions for time-dependent finite-wing motions."

This document details activities at the Hanford Engineer Works during the month of May 1949.

This report details events of importance reported by the Hanford Operations Office for the week ending June 15, 1949.

Progress is reported on the quartz fiber microbalance design and research. The mechanism for drawing the quartz fibers and the measurements of the properties of the fibers are described. Design and construction of a mass spectrograph and a cloud chamber is presented. Refilling B-wall tubes is investigated.