Triangular lifting wing in pitching and rolling with both subsonic and supersonic leading edges investigated and pressure coefficients obtained; family of thin sweptback triangular wings having symmetrical thickness distribution also investigated.
Generalized linearized conical flow
NACA -- Tech Note
1952
48 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Linearized supersonic theory of conical wings
Engineering Index Backfile | 1948
|Linearized supersonic theory of conical wings
NTRS | 1950
|Some conical and quasi-conical flows in linearized supersonic-wing theory
Engineering Index Backfile | 1950
|Wiley | 2012
|