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UNSTEADY SUBSONIC AND TRANSONIC POTENTIAL FLOW OVER HELICOPTER ROTOR BLADES

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BookPublisher: Nasa, Washington, D.C. 1974Description: 28.DDC classification: NASA | CR-2463

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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 CR-2463 (Browse shelf)	Not for loan		TR12864

Total holds: 0

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Previous	NASA CR-2460 A SYSTEM TO GEOMETRICALLY RECTIFY AND MAP AIRBORNE SCANNER IMAGERY AND TO ESTIMATE GROUND AREA	NASA CR-2461 CAPACITANCE DISCHARGE SYSTEM FOR IGNITION OF SINGLE BRIDGE APOLLO STANDARD INITIATORS (SBASI)	NASA CR-2462 ANALYSIS OF DYNAMIC STALL USING UNSTEADY BOUNDARY-LAYER THEORY	NASA CR-2463 UNSTEADY SUBSONIC AND TRANSONIC POTENTIAL FLOW OVER HELICOPTER ROTOR BLADES	NASA CR-2464 A GENERAL THEORY OF UNSTEADY COMPRESSIBLE POTENTIAL AERODYNAMICS	NASA CR-2467 - LOW-SPEED TEST OF TRANSLATING LIP AXISYMMETRIC INLETS FOR SUBSONIC TRANSPORTS	NASA CR-2468 - FULL-SCALE FIRE PROGRAM TO EVALUATE NEW FURNISHINGS AND TEXTILE MATERIALS DEVELOPED BY THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION	Next

Bound With Nasa Cr-2459-2462,2464

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