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THE SUPERSONIC THICKNESS DRAG OF RECTANGULAR WINGS WITH LINEAR SPANWISE TAPER IN THICKNESS

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Material type: Text

TextPublication details: Douglas, Santa Monica 1953Description: 22DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	DOUGLAS SM-14739 (Browse shelf(Opens below))	Not for loan		TR2983

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	D-6403 FORMULAS FOR NTH ORDER DERIVATIVES OF HYPERBOLIC AND TRIGONOMETRIC FUNCTIONS	D-6405 EXAMINATION OF BOUNDARY CONDITIONS FOR HEAT TRANSFER THROUGH A POROUS WALL	DOUGLAS SM-14735 EFFECT OF AIRCRAFT JET ENGINE EXHAUST IMPINGING ON AIRFIELD SURFACE	DOUGLAS SM-14739 THE SUPERSONIC THICKNESS DRAG OF RECTANGULAR WINGS WITH LINEAR SPANWISE TAPER IN THICKNESS	DOUGLAS SM-14885 SMALL SCALE TESTS ON JET ENGINE PEBBLE ASPIRATION	DOUGLAS SM-14976 SOME AERODYNAMIC CHARACTERISTICS OF WIDE-DELTA CRUCIFORM WINGS WITH CANARD-DELTA OR TRAILING-EDGE CONTROL SURFACE	DOUGLAS SM-14991 A PRELIMINARY THEORETICAL INVESTIGATION OF THE EFFECTS OF PROPERLLER SLIPSTREAM ON WING LIFT	Next

Bound With Dougals Sm-14735,14885,14973,14976,14991

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