GJB 6611-2008
Test method of helicopter rotor model in low speed wind tunnel (English Version)

Standard No.

GJB 6611-2008

Language

Chinese, Available in English version

Release Date

2008

Published By

Military Standard of the People's Republic of China-General Armament Department

Latest

GJB 6611-2008

Scope

This standard specifies the basic method for helicopter conventional rotor model tests in low-speed wind tunnels. This standard applies to helicopter rotor model tests conducted in low-speed wind tunnels. Rotor model tests carried out in other test sites can refer to this standard.

GJB 6611-2008 Referenced Document

• GJB 1179 High-speed wind tunnel and low-speed wind tunnel flow field quality specifications
• GJB 3209 helicopter terminology
• GJB 4296 Wind tunnel testing terminology and symbols
• GJB 4395-2002 Aerospace vehicle low-speed wind tunnel force measurement test method
• GJB 5202-2003 General requirements for helicopter rotor wind tunnel testing
• GJB 567A Rules for Preparing China National Defense Science and Technology Reports

GJB 6611-2008 history

• 2008 GJB 6611-2008 Test method of helicopter rotor model in low speed wind tunnel