FIELD: experimental aerodynamics. SUBSTANCE: method involves the steps of: fixing model 1 in a working portion of wind tunnel, producing a steady flow with predetermined parameters, measuring aerodynamic loads upon model 1 and parameters of jet 12 outgoing from flow-throw duct 3 and measuring aerodynamic loads upon stern portion 5 of model 1. The method is characterized in that model 1 which is affixed to side holder 5 and stern portion 5 of which is attached to the main one through intramodel strain-gauge scales 9 with air intake 2 working and air intake 2 closed by plug 10 is additionally tested but at simulating the operation of a jet engine by feeding compressed air to nozzle 4 through duct 11 inside holder 6 at equality of pressure in the outlet cross-section of nozzle 4 in these two tests. The difference of loads acting upon stern portion 5 of model 1 which is subtracted from the load upon model 1 determined from extrapolation. EFFECT: enhanced reliability and accuracy. 3 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
STING FOR TEST IN WIND TUNNEL ON ELECTROMECHANICAL BALANCE | 1993 |
|
RU2114409C1 |
JET ENGINE IMITATORS CALIBRATION STAND | 1992 |
|
RU2009457C1 |
METHOD OF MEASUREMENT OF AERODYNAMIC CHARACTERISTICS OF MODEL OF FLYING VEHICLE AND DEVICE FOR ITS IMPLEMENTATION | 1994 |
|
RU2084851C1 |
METHOD OF CONDUCTING AERODYNAMIC TESTS ON MODEL AIRCRAFT AND STAND FOR REALISING SAID METHOD | 2009 |
|
RU2421701C1 |
ACTIVE SYSTEM FOR CONTROL OF LIFTING FORCE | 1994 |
|
RU2086469C1 |
SILENCING NOZZLE OF AIR-JET ENGINE | 1993 |
|
RU2092708C1 |
GEAR FOR ANGULAR AND LINEAR MOVEMENT OF MODEL OF AIRCRAFT IN WIND TUNNEL | 1994 |
|
RU2102714C1 |
AIRCRAFT | 1993 |
|
RU2076826C1 |
METHOD OF CREATION OF THRUST OF JET ENGINE AND DEVICE FOR REALIZATION OF THIS METHOD | 1995 |
|
RU2103538C1 |
FAIRING OF EXTENSION AND RETRACTION MECHANISM FOR EXTENSION FLAPS | 1995 |
|
RU2085441C1 |
Authors
Dates
1994-11-15—Published
1989-07-26—Filed