Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method,

"CM-1034."

The finite range Wiener-Hopf integral equation and a boundary value problem in a waveguide /

"Contract No. AF33(616)-6079 Project No. 9-(13-6278) Task 40572. Sponsored by: Wright Air Development Center"

Elements of the differential and integral calculus, by a new method, founded on the true system of Sir Isaac Newton, without the use of infinitesimals or limits.

Mode of access: Internet.

An iterative method for solving nonsymmetric linear systems with dynamic estimation of parameters /

Vita.