Linearized slender body theory is applied to computation of aerodynamic forces on oscillating, or deforming, body of revolution; time dependence is taken to be sinusoidal; apparent mass approximation is obtained for body of small radius; specific calculations are performed for body in rigid motion.
Unsteady aerodynamic forces on slender body of revolution in supersonic flow
NASA -- Tech Note
1961
32 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Unsteady aerodynamic forces on slender supersonic aircraft with flexible wings and bodies
Engineering Index Backfile | 1963
|Flow over slender body of revolution at supersonic velocities
Engineering Index Backfile | 1946
|Flow over a slender body of revolution at supersonic velocities
TIBKAT | 1946
|