GJB 6758-2009
Test method of pressure measurement in conventional hypersonic wind tunnel (English Version)

Standard No.

GJB 6758-2009

Language

Chinese, Available in English version

Release Date

2009

Published By

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

Latest

GJB 6758-2009

Scope

This standard specifies the basic requirements, test procedures, test data processing and evaluation of conventional supersonic wind tunnel aircraft model pressure test. This standard is applicable to the steady pressure measurement test on the surface of conventional hypersonic wind tunnel aircraft model with Mach number 5~10.

GJB 6758-2009 Referenced Document

• GJB 2987 Hypersonic Wind Tunnel Model Design Guidelines Modification Sheet 1-2015*， 2015-12-19 Update
• GJB 4296 Wind tunnel testing terminology and symbols
• GJB 4297 Wind tunnel force measurement, pressure measurement and thermal test information collection requirements
• GJB 4399-2002 Hypersonic wind tunnel aerodynamic test method
• GJB 567A-1997 Rules for Preparing China National Defense Science and Technology Reports

GJB 6758-2009 history

• 2009 GJB 6758-2009 Test method of pressure measurement in conventional hypersonic wind tunnel