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IMPLOSION DRIVEN HYPERVELOCITY LAUNCHER PERFORMANC USING GASEOUS DETONATION WAVES

By: Watson,J. D.

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BookSeries: University Of Toronto Institute For Aerospace Studies Tn No.113. Publisher: University Of Toronto, Toronto 1967Description: 26.DDC classification: TR | IAS-113

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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 IAS-113 (Browse shelf)	Not for loan		TR5072

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

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Previous	TR IAS-110 REFRACTION OF SOUND BY JET FLOW AND JET TEMPERATURE II	TR IAS-111 ATTEMPT TO CORRELATE BIMODAL FATIGUE ENDURANCE DISTRIBUTIONS IN OFHC COPPER WITH WOOD'S H,F AND S RANGES	TR IAS-112 STATISTICAL ASPECTS OF COEXISTING FATIGUE FAILURE MECHANISMS IN OFHC COPPER	TR IAS-113 IMPLOSION DRIVEN HYPERVELOCITY LAUNCHER PERFORMANC USING GASEOUS DETONATION WAVES	TR IAS-114 DISCONTINUOUS SOLUTIONS FOR NONEQUILIBRIUM SUPERSONIC FLOWS	TR IAS-115 RESPONSE OF A CYLINDRICAL STRUCTURE TO A TURBULENT FLOW FIELD AT SUBCRITICAL REYNOLDS NUMBER	TR IAS-116 Study of a neon cycle cryogenic pumping system for a low density plasma tunael	Next

Bound With:Ias Ut 110-116

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