Normal view MARC view ISBD view

MODIFIED VELOCITY DEFECT LAW FOR TURBULENT BOUNDARY LAYERS WITH INJECTION

Material type: materialTypeLabel

BookSeries: College Of Aeronautics Report No,170. Publisher: College Of Aeronautics, Cranfield Edition: 1967.Description: 10.DDC classification: TR | COA-194

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	TR COA-194 (Browse shelf)	Not for loan		TR3003

Total holds: 0

Previous								Next
Previous	TR COA-177 CALIBRATION OF THE FLOW IN THE CHANNEL OF THE WHIRLING ARM	TR COA-18 Design and construction of a weld heat-affected zone simulator	TR COA-19 Welding embrittlement of the parent plate outside the visible heat affected zone region	TR COA-194 MODIFIED VELOCITY DEFECT LAW FOR TURBULENT BOUNDARY LAYERS WITH INJECTION	TR COA-195 NEW CLASS OF SUBHARMONIC SOLUTIONS TO DUFFING'S EQUATION	TR COA-196 STABILITY OF GROUND EFFECT WINGS	TR COA-198 "TURBOCODE" SCHEME FOR THE PROGRAMMING OF THERMODYNAMIC CYCLE CALCULATIONS ON AN ELECTRONIC DIGITAL COMPUTER	Next

Bound With: Coa Rep Aero No.170-199

There are no comments for this item.

PKK Library