Accession Number : AD0421685

Title :   LEADING EDGES DEVELOPMENT - DYNA SOAR. VOLUME III THERMAL GRADIENT AND LOADS TEST DATA,

Corporate Author : BOEING CO SEATTLE WASH

Personal Author(s) : Bowers,D. A. ; Esch,Paul G.

Report Date : 25 JUN 1963

Pagination or Media Count : 1

Abstract : Contents: tabulated temperature data, tabulated pressure load vs. deflection data, tabulated pressure load vs. maximum shear stress and principal stress data, rapid load vs. time curves, tabulated rapid load vs. deflection data, tabulated slow load vs. deflection data, and tolerances for thermocouples.

Descriptors :   (*BOOST GLIDE VEHICLES, LEADING EDGE FLAPS), MANNED SPACECRAFT, AERODYNAMIC LOADING, TEMPERATURE, LOAD DISTRIBUTION, PRESSURE, DEFLECTION, SHEAR STRESSES, TIME, THERMOCOUPLES, EXPERIMENTAL DATA, TABLES(DATA), AERODYNAMIC HEATING, DELTA WINGS

Distribution Statement : APPROVED FOR PUBLIC RELEASE