Airplane Stability for Flight with Constant Angular Velocity around the Longitudinal Axis,

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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

Author(s):
Pastrakuljic, Milorad
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Nauchno-Tehnicki Pregled (Yugoslavia) v20 n5 p37-41 1970.
Annotation:
Airplane Stability for Flight with Constant Angular Velocity around the Longitudinal Axis--Translation.
Pagination:
0011

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HC-23-829-71
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
(*AERODYNAMICS, STABILIZATION SYSTEMS), ACCELERATION, FLIGHT PATHS, AERODYNAMIC LOADING, EQUATIONS, CENTER OF GRAVITY, AIRCRAFT, STABILITY, YUGOSLAVIA
Field(s)/Group(s):
Fluid Mechanics
Keyword(s):
TRANSLATIONS
Report Date:
1971 Nov 29