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Elevated stagnation temperature and strain gauge balances in the instrumentation of a supersonic wind tunnel

By: G P Tonkin.

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BookPublisher: DDC classification: NATO | AGARD R-15

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NATO AGARD R-15 (Browse shelf)	Not for loan		TR16651

Total holds: 0

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Previous	NATO AGARD R-139 The light gas hypersonic gun tunnel at A.R.D.E. fort halstead, kent	NATO AGARD R-14 Mesure et enregistrement des mesures sur les balances aerodynamiques a jauges a fil resistant	NATO AGARD R-140 NACA hypersonic rocket and high-temperature jet facilities	NATO AGARD R-15 Elevated stagnation temperature and strain gauge balances in the instrumentation of a supersonic wind tunnel	NATO AGARD R-16 Automatic indicating and recording data systems for wind tunnels	NATO AGARD R-17 High speed systems of wind tunnel data handling	NATO AGARD R-18 Short notes on model-making and force measuring techniques	Next

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