Name:
MODUK DEF STAN 00-970: PT 7: SEC 5 PDF
Published Date:
01/31/2007
Status:
[ Cancelled ]
Publisher:
British Defence Standards
INTRODUCTION
The requirements of this Leaflet are concerned with:
(i) The control of flutter, divergence, ground and air resonance and allied aeroelastic and aero-mechanical self-excited phenomena.
(ii) The restriction of structural distortion of the rotors, control systems and airframe within limits that will not dangerously impair stability and control.
Rotorcraft airframes and equipments are subjected to vibratory forcing from a number of sources. These forced response aspects of vibration are dealt with in Leaflet 501.
Compliance with the requirements shall be established by calculation or by compliance with the relevant criteria given in the Leaflets of this Leaflet, supported in each case by tests. Calculations shall be discussed with and approved by the Director, RAE.
| Edition : | I2 |
| File Size : | 1 file , 1.1 MB |
| Number of Pages : | 104 |
| Published : | 01/31/2007 |
