• Shopping Cart
    There are no items in your cart

DEFSTAN 00-970(PT7)SEC5/2(2007) : 2007

Withdrawn

Withdrawn

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 5: AERO-ELASTICITY AND VIBRATION

Available format(s)

PDF

Language(s)

English

Published date

01-01-2007

Withdrawn date

09-30-2014

US$20.00
Excluding Tax where applicable

LEAFLET 500 AERO-ELASTICITY
LEAFLET 501 VIBRATION AND INTERNAL NOISE
APPENDIX No 1 - Not Issued
APPENDIX No 2 - U.S. MILITARY SPECIFICATIONS,
                STANDARDS AND HANDBOOKS

Describes requirements concerned with: - The control of flutter, divergence, ground and air resonance and allied aero-elastic and aero-mechanical self-excited phenomena, - The restriction of structural distortion of the rotors, control systems and airframe within limits that will not dangerously impair stability and control.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT7)SEC5/1(2006). (03/2007)
DocumentType
Standard
Pages
99
PublisherName
UK Ministry of Defence Standards
Status
Withdrawn
Supersedes

ISO 2631:1978 Guide for the evaluation of human exposure to whole-body vibration
SAE J1013_199208 MEASUREMENT OF WHOLE BODY VIBRATION OF THE SEATED OPERATOR OF OFF-HIGHWAY WORK MACHINES

US$20.00
Excluding Tax where applicable