Formulas are derived for calculating coefficients of rotational derivatives of downwash in vortex sheet behind rear edge of harmonically oscillating rectangular and triangular wings; results of some numerical computations are given.
Unsteady downwash of supersonic flow at wing's rear edge
Nestatsionarnye skosy sverkhzvukovogo potoka u zadnei kromki kryla
1964
5 pages
Aufsatz (Zeitschrift)
Russisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Calculation of downwash behind supersonic wing
Engineering Index Backfile | 1949
|Online Contents | 1994
Note on evaluation of supersonic downwash integral
Engineering Index Backfile | 1954
|Line-vortex theory for calculation of supersonic downwash
Engineering Index Backfile | 1950
|