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BOUNDARY LAYER BLEED DRAG AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 19Description: 22.DDC classification: ARC | R&M-3529

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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	ARC R&M-3529 (Browse shelf)	Not for loan		TR12777

Total holds: 0

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Previous	ARC R&M-3522 REAL-AIR EFFECTS IN PROPELLING NOZZLES.	ARC R&M-3523 CALCULATION METHODS FOR THREE-DIMENSIONAL TURBULENT BOUNDARY LAYERS.	ARC R&M-3524 A PILOTED SIMULATOR STUDY OF THE TAKE-OFF MANOEUVRE OF A LARGE AIRCRAFT WITH AND WITHOUT A TAKE-OFF DIRECTOR.	ARC R&M-3529 BOUNDARY LAYER BLEED DRAG AT SUPERSONIC SPEEDS.	ARC R&M-3530 THE LAMINAR BOUNDARY LAYER ON AN INCLINED CONE.	ASA CR-2262 - BUMPER-PROTECTED LAMINATED SPACECRAFT MAINWALLS	\ASA CR-645 - EQUATIONS FOR THERMOELASTIC AND VISCOELASTIC CYLINDRICAL SAANDWICH SHELLS	Next

Bound With Arc R&M 3521-29.,3530.

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