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THEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW

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BookPublisher: Nasa, Washington, D.C. 1968Description: 76.DDC classification: NASA | TN D-4929

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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-4929 (Browse shelf)	Not for loan		TR12449

Total holds: 0

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Previous	NASA TN D-4926 DESIGN-POINT PERFORMANCE OF A DOUBLE-CONTAINMENT TANTALUM-AND-STAINLESS-STEEL MERCURY BOILER FOR SNAP-8	NASA TN D-4927 A STUDY OF STIFFNESS MATRICES FOR THE ANALYSIS OF FLAT PLATES	NASA TN D-4928 WIND-TUNNEL INVESTIGATION OF LARGE JET TRANSPORT MODEL EQUIPED WITH AN EXTERNAL-FLOW JET FLAP	NASA TN D-4929 THEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW	NASA TN D-4930 THE LOOG-A-POSTERIORI PROBABILITY METRIC FOR USE IN SEQUENTIAL DECODING	NASA TN D-4932 ELASTIC SCATTERING OF 21-MEV PROTONS FROM NITROGEN 14, OXYGEN 16, ARGON 40, NIKEL 58, AND TIN 116	NASA TN D-4933 EXCITED STATES OF BARIUM 136 AND BARIUM 134	Next

Bound With Nasa Tn D-4921-28, 4930.

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