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LONGMUIR PROBE MEASUREMENTS IN THE STAGNATION POINT BOUNDARY LAYER OF A BLUNT-NOSED BODY IN A SUPERSONIC PLASMA FLOW

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BookSeries: Institute Of Aerophysics Technical Note No.58. Publisher: University Of Toronto, Toronto 1963Description: 23.DDC classification: TR | IOA-58

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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	TR IOA-58 (Browse shelf)	Not for loan		TR5024

Total holds: 0

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Previous	TR IOA-55 INVESTIGATION OF THE OSCILLATORY DERIVATIVES OF AN AEROFOIL WITH FLAPS OSCILLATING NEGATIVE ANGLES OF ATTACK	TR IOA-56 CHARACTERISTICS OF A RECTANGULAR WING WITH A PERIPHERAL JET IN GROUND EFFECT	TR IOA-57 EXPERIMENTAL INVESTIGATION OF THE BEHAVIOUR OF STIFFENED PLATES IN AXIAL COMPRESSION	TR IOA-58 LONGMUIR PROBE MEASUREMENTS IN THE STAGNATION POINT BOUNDARY LAYER OF A BLUNT-NOSED BODY IN A SUPERSONIC PLASMA FLOW	TR IOA-59 CHARACTERISTICS OF A RECTANGULAR WING WITH A PERIPHERAL JET IN GROUND EFFECT	TR IOA-60 GYROSTABILIZATION OF ELLIPTIC WING WITH PERIPHERAL JET HOVERING IN GROUND EFFECT	TR IOA-61 ASYMMETRY OF ANNULAR JET FLOW IN GROUND PROXIMITY	Next

Bound With: Ioa Uot 53-61

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