The directional sensitivity of a constant temperature, thin, wall moun
ted hot-film gauge with respect to variations in yaw angle is investig
ated. Results obtained for the response of a hot-film gauge in a bound
ary layer flow fit the correlation between the effective cooling veloc
ity for a hot-wire gauge and the yaw angle suggested by other workers.
The yaw factor k(1)(2) used in this correlation is typically less tha
n 1.0. Results presented for the hot-film gauge in a boundary layer in
dicate that the yaw factor depends on both the distance into the bound
ary layer and the magnitude of the free stream velocity. At some veloc
ity, close to zero, the results predict a yaw factor greater than unit
y. Computer simulations using the k - epsilon turbulence model are pre
sented which verify this prediction. Yaw factors greater than one resu
lt because diffusion from the edges of the gauge becomes significant a
t low velocities with respect to the total heat transferred.