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TESTS ON PROBES DESIGNED TO MEASURE STAGNATION PRESSURE DIRECTLY IN A SUPSERSONIC STREAM

By: Mundell, A.R.G.

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BookSeries: Aeronautical Research Council Reports And Memoranda R&M 3755. Publisher: DDC classification: R&M3755

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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	R&M3755 (Browse shelf)	Not for loan		TR6188

Total holds: 0

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Previous	R&M3746 OCCURRENCE AND REMOVAL OF INDETERMINACY FROM FLOW CALCULATION IN TURBOMACHINES	R&M3753 LONGITUDINAL MOTIONS OF AIRCRAFT INVOLVING HIGH ANGLES OF ATTACK	R&M3754 EFFECT OF COMPRESSIBILITY ON UNSTALLED TORSIONAL FLUTTER	R&M3755 TESTS ON PROBES DESIGNED TO MEASURE STAGNATION PRESSURE DIRECTLY IN A SUPSERSONIC STREAM	R&M3756 SOME UNSEPARATED BASE FLOWS WITH HEAT ADDITION	R&M3757 FORM OF THE SUPERSONIC FLOW EQUATIONS FOR AN IDEAL GAS	R&M3758 ON THE APPLICATION OF SUBSONIC LINEARISED WING THEORY TO SECOND ORDER FORCES AND MOMENTS	Next

Bound With: R&M 3749-3759

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