MH
M.H.L. Hounjet
info
Please Note
This page displays the records of the person named above and is not linked to a unique person identifier. This record may need to be merged to a profile.
1 records found
1
Authored
A description is given of a computationally inqjroved potential gradient method to calculate unsteady aerodynamic derivatives in supersonic flow. Results are presented and comparisons are made with results of existing methods and with experimental data for a fighter-type wing.