We investigate the effect of buoyancy on the upper-branch linear stabi
lity characteristics of an accelerating boundary-layer how. The presen
ce of a large thermal buoyancy force significantly alters the stabilit
y structure. As the factor G (which is related to the Grashof number o
f the flow, and defined in Section 2) becomes large and positive, the
flow structure becomes two layered and disturbances are governed by th
e Taylor-Goldstein equation. The resulting inviscid modes are unstable
for a large component of the wavenumber spectrum, with the result tha
t buoyancy is strongly destabilizing. Restabilization is encountered a
t sufficiently large wavenumbers. For G large and negative the flow st
ructure is again two layered. Disturbances to the basic flow are now g
overned by the steady Taylor-Goldstein equation in the majority of the
boundary layer, coupled with a viscous wall layer. The resulting eige
nvalue problem is identical to that found for the corresponding case o
f lower-branch Tollmien-Schlichting waves, thus suggesting that the ne
utral curve eventually becomes closed in this limit.