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Thermophysics and Aeromechanics

2004 year, number 4

Review of methods for studying hypersonic gas flows past bodies with ablating coatings

N.I. Sidnyaev
Bauman State Technical University, Moscow, Russia
Pages: 489-508

Abstract

Means in most common use for reliable protection of aircraft surfaces against thermal loads are reviewed. Development of such means involves detailed consideration of mass-transfer processes on streamlined surfaces. Passive and active methods for thermal protection of surfaces are discussed, based on the use of ablating heat-shielding coatings. The review classifies studies, including those published recently, that confirm high efficiency and great potential of active heat-shielding systems for aircraft using forced blowing of coolants into boundary layer.