4.2 Static Precsvre TranSduCCr &3 uynamic Pressure Transduoer 4.4 Temperature Suwrtive Element
M.J.G. Cox, A.Id.1.E.E., k.M.i.1.E.E. The Llevelopent of an Air>iass Flow rate mter to oowx n wry wise range 1s describea which, ensertially WI analogue computer, sves a twosweep pointer direct prescnta%ion of sir mass flow rate, indepelldent of pressure, tompereturc and velocity changes within t...
Main Authors: | , , , |
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Other Authors: | |
Format: | Text |
Language: | English |
Published: |
1954
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Subjects: | |
Online Access: | http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.227.308 http://naca.central.cranfield.ac.uk/reports/arc/cp/0230.pdf |
Summary: | M.J.G. Cox, A.Id.1.E.E., k.M.i.1.E.E. The Llevelopent of an Air>iass Flow rate mter to oowx n wry wise range 1s describea which, ensertially WI analogue computer, sves a twosweep pointer direct prescnta%ion of sir mass flow rate, indepelldent of pressure, tompereturc and velocity changes within the range of the instzwmont. The pointers are driven by a servo system which is error-actuated from the computing briec network, secondly feedbackbeing employed to maintain stability wzth n saturated angular output rate of apprsrJmatelJ 330 per scoond. Specifkoatlons orid perfarmanoe figures are given for the mdivxdud transduoor e1ement.s snfi the complete indrument, error estimations ore made, and the servo stability is 6iscusscd.-l- 1 IdrWluction 2 XWnciple of iieasuroment 3 tiethod of Moaswement 4 l?escrlption |
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