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EFFECT OF REYNOLDS NUMBER ON THE LATERAL-STABILITY DERIVATIVES AT LOW SPEED OF SWEPTBACK- AND DELTA-WING-FUSELAGE COMBINATIONS OSCILLATING IN YAW

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BookPublisher: Nasa, Washington, D.C. 1960Description: 45.DDC classification: NASA | TN D-398

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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-398 (Browse shelf)	Not for loan		TR15931

Total holds: 0

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Previous	NASA TN D-3958 WEAR AND FRICTION OF IMPERGNATED MECHANICAL CARBONS AT TEMPERATURES TO 1400 DEGREE F (760 DEGREE C) IN AIR OR NITROGEN	NASA TN D-396 SOME EXPERIMENTS CONCERNING SUBSEQUENT YIELD SURFACES	NASA TN D-397 DATA FROM A STATIC-THRUST INVESTIGATION OF A LARGE-SCALE GENERAL RESEARCH VTOL-STOL MODEL IN GROUND EFFECT	NASA TN D-398 EFFECT OF REYNOLDS NUMBER ON THE LATERAL-STABILITY DERIVATIVES AT LOW SPEED OF SWEPTBACK- AND DELTA-WING-FUSELAGE COMBINATIONS OSCILLATING IN YAW	NASA TN D-399 VARIATION IN HEAT TRANSFER DURING TRANSIENT HEATING OF A HEMISPHERE AT A MACH NUMBER OF 2	NASA TN D-4 INFLUENCE OF SHAFT DEFLECTION AND SURFACE ROUGHNESS ON LOAD-CARRYING CAPACITY OF PLAIN JOURNAL BEARINGS	NASA TN D-400 ANALYSIS OF FRAME-REINFORCED CYLINDRICAL SHELLS PART 1- BASIC THEORY	Next

Bound With Nasa Tn D-391-97,399-400

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