GJB 6753-2009
Test method for powered model of propeller driven aircraft in low speed wind tunnel (English Version)
- Standard No.
- GJB 6753-2009
- Language
- Chinese, Available in English version
- Release Date
- 2009
- Published By
- Military Standard of the People's Republic of China-General Armament Department
- Status
- 2016-03
- Replace By
- GJB 6753-2009(XG1-2015)
- Latest
- GJB 6753-2009(XG1-2015)
- Scope
- This standard specifies the basic methods for dynamic model tests on propeller aircraft. This standard is applicable to the dynamometric test for measuring the influence of the pull-in propeller model slipstream on the full-model aerodynamic characteristics of the aircraft in a low-speed wind tunnel. Physical propeller slipstream influence test, propeller aerodynamic characteristic test, propeller slipstream influence test on aircraft component aerodynamic characteristics, propulsion propeller slipstream influence test, other propeller slipstream influence tests and related propeller slipstream Pressure test can also refer to the use.
GJB 6753-2009 Referenced Document
- GB/T 16638.4 Aerodynamics.Concepts,quantities and symbols.Part 4:Aerodynamic forces,moments,their coefficients and derivatives of aircraft
- GB/T 9239-1988 Balance quality of rigid rotors--Determination of permissible residual unbalance
- GJB 1061-1991 Accuracy index of high-speed wind tunnel and low-speed wind tunnel force measurement experiments
- GJB 180 Design specifications for low-speed wind tunnel aircraft models
- GJB 2244 Specification for wind tunnel strain balances
- GJB 4395-2002 Aerospace vehicle low-speed wind tunnel force measurement test method
- GJB 567 Rules for Preparing National Defense Science and Technology Reports
GJB 6753-2009 history
- 0000 GJB 6753-2009(XG1-2015)
- 2009 GJB 6753-2009 Test method for powered model of propeller driven aircraft in low speed wind tunnel
