摘 要: | RenBinWiththeadventofnewfighterandmissileprojects,aneedforimproveddynamictestingofwindtunnelmodelsaroseatCARDCinthetransonicspeedrangs.Soduringlastfiveyears,newforcedoscillationapparatusandmeasurementsystemusedtomeasurebothrolldampingandpitch/yawdampingin1.2m×1.2mtransonicwindtunnelhavebeendeveloped.Theapparatusincludeapitch/yawoscillationbalanceandarolloscillationbalance.InNovemberl995,wefinishedthewindtunnelverificationtestsoftheStandardDynamicsModel(SDM),asimplifiedfighteraircraftmod…
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