Accession Number : AD0428616


Title :   AERODYNAMIC HEATING AND STRUCTURAL TEMPERATURE RESPONSE


Corporate Author : HERCULES POWDER CO CUMBERLAND MD ALLEGANY BALLISTICS LAB


Personal Author(s) : Browning, Stanley C


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/428616.pdf


Report Date : Jul 1963


Pagination or Media Count : 71


Descriptors :   *SUPERSONIC FLIGHT , UNDERWATER TO SURFACE MISSILES , TEMPERATURE , STABILITY , ENERGY , BOUNDARY LAYER , CONVECTION , THERMAL CONDUCTIVITY , SOUND , HIGH ALTITUDE , SUPERSONIC FLOW , AIR TO AIR MISSILES , ROCKET ENGINE CASES , SURFACE TEMPERATURE , LAMINAR FLOW , SOLID PROPELLANT ROCKET ENGINES , THERMAL RADIATION , EQUATIONS OF STATE , THERMAL INSULATION , ATMOSPHERICS , VELOCITY , HEAT TRANSFER


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE