Accession Number:
AD0738231
Title:
Airplane Stability for Flight with Constant Angular Velocity around the Longitudinal Axis,
Descriptive Note:
Corporate Author:
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s):
Report Date:
1971-11-29
Pagination or Media Count:
11.0
Abstract:
The paper considers the effects of longitudinal acceleration and magnus forces and moments on stability of aircraft having single plane of symmetry and gives expressions allowing estimation of cases when such effects should be taken into account. Author
Descriptors:
Subject Categories:
- Fluid Mechanics