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

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE