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AN INVESTIGATION OF TRANSITION FIXING TECHNIQUE FOR A 10.5% THICK, 28 DEGREE SWEPTBACK WING AT HIGH SUBSONIC SPEEDS AND R~=3.10 TO THE POWER 6.

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BookPublisher: Her Majesty'S Stationery Office,London 1972Description: 42.DDC classification: ARC | C.P. 1215

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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 C.P. 1215 (Browse shelf)	Not for loan		TR10591

Total holds: 0

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Previous	ARC C.P. 1208 BOUNDARY-LAYER PRESSURE FLUCTUATIONS AT HIGH REYNOLDS NUMBERS ON A FREE-FLIGHT TEST VEHICLE.	ARC C.P. 1212 HEAT TRANSFER AND SURFACE PRESSURE MEASUREMENTS ON TWO CONICAL WINGS IN FREE FLIGHT UP TO M SUFFIX INFINITE=4.5	ARC C.P. 1213 SOME MODIFICATIONS TO THE CALCULATION METHOD FOR WINGS WITH PART-SPAN EXTENDING-CHORD FLAPS GIVEN IN RAE TECHNICAL REPORT 69034.	ARC C.P. 1215 AN INVESTIGATION OF TRANSITION FIXING TECHNIQUE FOR A 10.5% THICK, 28 DEGREE SWEPTBACK WING AT HIGH SUBSONIC SPEEDS AND R~=3.10 TO THE POWER 6.	ARC C.P. 1216 FORTRAN PROGRAMMES FOR AXISYMMETRIC POTENTIAL FLOW AROUND CLOSED AND SEMI-INFINITE BODIES.	ARC C.P. 1217 A COMPUTER PROGRAM TO CALCULATE THE PRESSURE DISTRIBUTION ON AN ANNULAR AEROFOIL.	ARC C.P. 1218 AN EXAMINATION OF AN ITERATIVE PROCEDURE FOR DETERMINING THE CHARACTERISTIC EXPONENTS OF LINEAR DIFFERENTIAL EQUATIONS WITH PERODIC COFFICIENTS.	Next

Bound With C.P.1211-14 And 1216-20

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