Normal view MARC view ISBD view

A COMPUTER PROGRAM TO CALCULATE THE PRESSURE DISTRIBUTION ON AN ANNULAR AEROFOIL.

Material type: materialTypeLabel

BookPublisher: Her Majesty'S Stationery Office,London 1972Description: 54.DDC classification: ARC | C.P. 1217

average rating: 0.0 (0 votes)

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. 1217 (Browse shelf)	Not for loan		TR10593

Total holds: 0

Previous								Next
Previous	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.	ARC C.P. 1219 THE DESIGN OF HIGH SENSITIVITY PRESSURE TRANSDUCERS FOR USE IN SHOCK-TUNNELS.	ARC C.P. 1220 ANDOVER C. MK.1 AIRFIELD CRITERIA TRIALS.	Next

Bound With Arc C.P.1211-16 And 1218-20

There are no comments for this item.

PKK Library