J. Edward Anderson

Studies based on the Rankine-Hugoniot relations have classified MHO shock waves as fast, switch-on, intermediate, switch-off, and slow. Any waves found in nature must also: (a) possess steady-state structures and (b) be stable in the presence of small-flow disturbances. In this monograph, Dr. Anderson examines these criteria in relation to plane shocks for which the collision frequency is large compared with cyclotron frequency. It contains a three-dimensional graphic representation of shock end states and presents an exact solution for the shock adiabatic curve in a convenient form. An MIT Press Research Monograph.

Magnetohydrodynamic Shock Waves

Manuel Stein

John M. Hedgepeth

The structural analysis of arbitrary solid cantilever wings by thin-plate theory is reduced to the solution of linear ordinary differential equations by use of the assumption that the chordwise deflections may be expressed in the form of a power series. With the series limited to the first two and the first three terms, the differential equations are solved exactly for several samples of solid delta wings. For cases for which exact solutions to the differential equations cannot be obtained, a numerical procedure is derived. Some experimental data are presented and are found to compare favorably with the present theory.

Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form with Particular Reference to Delta Wings

John P. Reeder

United States. National Advisory Committee for Aeronautics

Ralph W. Stone

Almer D. Crim

Donald R. Bellman

Franklin A. Diedrich

Franklin K. Moore

Henry A. Pearson

I. Irving Pinkel

Kenneth A. Foss

Franklin W. Diedrich

G. Merritt Preston

Jack C. Humphrey

Gerard J. Pesman

James B. Whitten

John M. Hedgepath

Theodore Male

Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings

J. Edward Anderson

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