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THE LEADING-EDGE BUCKLING OF A THIN BUILT-UP WING DUE TO AERODYNAMIC HEATING.

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BookPublisher: Her Majesty'S Stationery Office, London 1961Description: 24.DDC classification: ARC | R&M 3295

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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 3295 (Browse shelf)	Not for loan Untraceable		TR11089

Total holds: 0

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Previous	ARC R&M 3292 FURTHER RESULTS ON THE MIXING OF FREE AXIALLY-SYMMETRICAL JETS OF MACH NUMBER 1.40	ARC R&M 3293 CHARTS OF PEAK AMPLITUDES IN INCIDENCE AND SIDESLIP IN ROLLING MANOEUVRES DUE TO INERTIA CROSS COUPLING	ARC R&M 3294 MEASUREMENT OF THE PITCHING-MOMENT DERIVETIVES FOR RIGID TAPERED WINGS OF HEXAGONAL PLANFORM OSCILLATING IN SUPERSONIC FLOW.	ARC R&M 3295 THE LEADING-EDGE BUCKLING OF A THIN BUILT-UP WING DUE TO AERODYNAMIC HEATING.	ARC R&M 3296 A PRELIMINARY DATA REPORT ON GROUND PRESSURE DISTURBANCES PRODUCED BY THE FAIREY DELTA 2 IN LEVEL SUPERSONIC FLIGHT.	ARC R&M 3297 NOTE ON THE EVALUATION OF SOLID-BLOCKAGE CORRECTIONS FOR RECTANGULAR WIND TUNNELS WITH SLOTTED WALLS.	ARC R&M 3298 CALCULATION OF STABILITY DERIVATIVES FOR TAPERED WINGS OF HEXAGONAL PLANFORM OSCILLATING IN A SUPERSONIC STREAM.	Next

Bound With Arc R&M3291-94, 3296-99

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