Highly localized heating rates occur in extreme thermal environments, such
as shock-shock interaction at hypersonic speeds. Experimental estimation of
heat Bur usually involves measurement of discrete unsteady surface tempera
tures on low conductivity materials that are chosen to reduce conduction ef
fects. Typically, temperature measurements are reduced to heat fluxes using
one-dimensional conduction techniques. However, lateral conduction from lo
calized high heat Bur regions into low heat Bur regions is significant and
influences the one-dimensional solution. The one-dimensional solution also
suffers mathematical instabilities. To evaluate the nonuniform, unsteady su
rface flux from measured temperatures, an inverse technique was devised tha
t damps instabilities in the temporal direction and resolves large and sudd
en flux changes in the spatial direction. Based on previous work, a simple
inverse method was used in time, and a function specification method was us
ed in space. Furthermore, a technique was devised to expedite the solution
by marching in space as well as in time. The new multidimensional inverse m
ethod was found to resolve steep spatial gradients more accurately in Bur t
han a one-dimensional method. Furthermore, the inverse procedure exhibits b
etter stability than a multidimensional forward technique.