Aerodynamic Heating of ParachutesWright Air Development Center, Air Research and Development Command, U.S. Air Force, 1957 - Aerodynamic heating - 53 pages |
Common terms and phrases
acetate acid after-shock flow air stream Alloy Amonium analysis anthraquinone Assuming assumption average heating rate beachloroethane beat benzoic acid BOILING boundary condition boundary layer calculated circular leading edge cloth Compounds Not Hydrates conductivity costing considered couting density dibromo discussed distance equation ethyl experimental feet Fist Ribbon flow pattern forward stagnation point front opening gives glycerol heat flux heat influx heat input heat transfer Hence high conductivity coating hout Hydrated Compounds hydroxy ideal gas incompressible flow Mach numbers mass transfer material metal methods Naphthalene nylon webbing obtained ORGANIC COMPOUNDS permeability phenyl plotted POINTS OF ORGANIC polyurethane porosity problem rate of evaporation ribbon parachute rute shell shown in Figure silicone solid specific stagnation temperature steady striking the surface subl sublining succinic acid supersonic stream surface held surface temperature temperature distribution temperature profiles thickness total heat various WADC