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FL-10 open test section flow calibrated

FL-10 open test section flow calibrated
Release time：
2019-05-28 10:16
Abstract:
FL-10opentestsectionflowcalibratedTheflowcalibrationwascompletedintheopentestsectionofFL-10windtunnelinMarch2019.Themaximumwindspeedcanreach85m/s,thedynamicpressurestabilityis0.0035andtheturbulenceis0
FL-51 high angle of attack force testing system

FL-51 high angle of attack force testing system
Release time：
2019-01-09 08:48
Abstract:
Afterappliedinseveralresearchprograms,thehighangleofattacktestingsystemwasadoptedinoneforcetestcampaignperformedinFL-51windtunnelinJuly,2018fortheindustrycustomer.Itsresultishighlyrecognized. FL-51windtunnelisacontinuouslowspeedwindtunnelwithopenandclosedinterchangeabletestsections.Thehighangleofattacktestingsystemcanbeusedintheopentestsection.Itsfeaturesareasfollows:Incidence:from-110°to110°Sideslipangle:from-38°to38°Velocity:from20m/sto70m/sSupport:Rearsupport,ventralsupport,dorsalsupport        FL-51highangleofattackforcetestingsystem
Half model force test capability built in FL-10 wind tunnel

Half model force test capability built in FL-10 wind tunnel
Release time：
2019-01-09 08:47
Abstract:
Half model test capability has been built in FL-10 wind tunnel. In September 2018, one civil UAV half model force test was successfully completed in FL-10 wind tunnel using handing basket type half model supporting system.
Free flight test performed in large FL-10 wind tunnel of AVIC ARI

Free flight test performed in large FL-10 wind tunnel of AVIC ARI
Release time：
2019-01-09 08:36
Abstract:
IcingwindtunneltestonthesensoroftransportaircrafthasbeensuccessfullycompletedinFL-61whichisa0.6mcontinuoustransonicwindtunnelofAVICARIatShenyang.ThetestwascarriedoutinMayandwasusedinthecertificationoftheaircraftsensorundericingconditions.FL-61windtunnelwasreviewedbyrepresentativesofFAAandCAACandwasacceptedtogenerateicingcertificationdatafortheaircraftsensor.StableicingconditionsweregeneratedinFL-61duringthetesttoverifythesensoranti-icingcapabilitiesundercontinuousmaximumicingconditionsfor45minutesandintermittentmaximumicingconditions.RepresentativesofFAAandCAACwitnessedthetestprocessandacceptedthedatageneratedforuseinthecertificationoftheaircraftsensor.Thisisthefirsttimeforthefacility,instrumentationandproceduresofFL-61toberecognizedbytheairworthinessauthoritiesandcustomerstoproduceacceptabledataforcertificationsinceitisputintousein2016.AndAVICARIcanprovideittocustomerstosupportcivilaircraftsandcomponentsinicingcertification.
New 2.0m acoustic wind tunnel put into use at AVIC ARI

New 2.0m acoustic wind tunnel put into use at AVIC ARI
Release time：
2019-01-09 08:35
Abstract:
After three years of construction, a new 2.0m acoustic wind tunnel (FL-52), which is located in Harbin, China, has been put into use in November, 2018. FL-52 wind tunnel is an aeroacoustic circuit wind tunnel with a closed-wall test section and an open jet.
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