Method for calculation of aerodynamic forces on oscillating combination of wing and fin is described; method is based on linearized theory and constitutes extension of method previously developed for isolated finite wings, indexed in Engineering Index 1959 p 24; results are given for 3 particular rigid modes and for Mach numbers 0 and 0.8.
Aerodynamic forces on combination of wing and fin oscillating in subsonic flow
Svenska Aeroplan Aktiebolaget -- Tech Note
1964
36 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Aerodynamic forces on rectangular wings oscillating in subsonic flow
Engineering Index Backfile | 1960
|Unsteady aerodynamic loading computation for subsonic oscillating wing
British Library Online Contents | 1995
|