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MAXIMUM LIFT-DRAG-RATIO CHARACTERISTICS OF RECTANGULAR AND DELTA WINGS AT MACH 6.9

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BookPublisher: Nasa, Washington, D.C. 1965Description: 46.DDC classification: NASA | TN D-2925 -

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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	NASA TN D-2925 - (Browse shelf)	Not for loan		TR8622

Total holds: 0

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Previous	NASA TN D-2922 - EFFECTS OF ASPECT RATIO AND CANOPY SHAPE ON LOW-SPEED AERODYNAMIC CHARACTERISTICS OF 50.0(DEGREE) SWEPT PARAWINGS	NASA TN D-2923 - FLIGHT EVALUATION OF THE X-15 BALL-NOSE FLOW-DIRECTION SENSORAS AN AIR-DATA SYSTEM	NASA TN D-2924 - HEAT-TRANSFER AND PRESSURE DROP CORRELATIONS FOR HYDROGEN AND NITROGEN FLOWING THROUGH TUNGSTEN WIRE MESH AT TEMPERATURES TO 5200(DEGREE) R	NASA TN D-2925 - MAXIMUM LIFT-DRAG-RATIO CHARACTERISTICS OF RECTANGULAR AND DELTA WINGS AT MACH 6.9	NASA TN D-2926 - STRUCTURAL BEHAVIOR AND BUCKLING STRENGTH OF HONEYCOMB SANDWICH CYLINDERS SUBJECTED TO BENDING	NASA TN D-2927 - TRANSONIC INVESTIGATION OF BASE PRESSURE ASSOCIATED WITH SHALLOW RHREE-DIMENSIONAL REARWARD-FACING STEPS	NASA TN D-2928 - WIND-TUNNEL PRESSURE MEASUREMENTS IN THE WAKE OF A CONE-CYLINDER MODEL AT MACH NUMBERS OF 2.30 AND 4.65	Next

Bound With Nasa Tn D-2921-30

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