Determination of stability derivatives of isolated rigid tail assemblies in sideslip and steady roll
2nd International Symposium on the Technology and Science of Low Speed and Motorless Flight ; 1974 ; Cambridge , MA , U.S.A.
1974-01-01
Conference paper
Electronic Resource
English
ENGINEERING NOTES - Maximum Steady Roll Rate in Zero-Sideslip Roll Maneuvers of Aircraft
Online Contents | 2002
|