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COMPARISON OF MEASURED FLAPWISE STRUCTURAL BENDING MOMENTS ON A TEETERING ROTOR BLADE WITH RESULTS CALCULATING FROM THE MEASURED PRESSURE DISTRIBUTION

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BookPublisher: Nasa, Washington, D.C. 1959Description: 32.DDC classification: NASA | MEMO 2-28-59L -

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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 MEMO 2-28-59L - (Browse shelf)	Not for loan		TR7547

Total holds: 0

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Previous	NASA MEMO 2-26-59A - SOME FINITE DIFFERENCE SOLUTIONS OF THE LAMINAR COMPRESSIBLE BOUNDARY LAYER SHOWING THE EFFECTS OF UPSTREAM TRANSPIRATION COOLING	NASA MEMO 2-27-59A - LOW-SPEED TESTS OF SEMISPAN-WING MODELS AT ANGLES OF ATTACK FROM 0(DEGREE) TO 180(DEGREE)	NASA MEMO 2-27-59E DETAILS OF EXACT LOW PRANDTL NUMBER BOUNDARY-LAYER SOLUTIONS FOR FORCED AND FOR FREE CONVECTION	NASA MEMO 2-28-59L - COMPARISON OF MEASURED FLAPWISE STRUCTURAL BENDING MOMENTS ON A TEETERING ROTOR BLADE WITH RESULTS CALCULATING FROM THE MEASURED PRESSURE DISTRIBUTION	NASA MEMO 2-5-59E AN EQUATION FOR THE MEAN VELOCITY DISTRIBUTION OF BOUNDARY LAYERS	NASA MEMO 2-6-59E PERFORMANCE OF SEVERAL INLET-BYPASS SYSTEMS FOR MATCHING A TWO-DIMENSIONAL VARIABLE-GEOMETRY MACH 3.0 INLET AT MACH 1.5 AND 2.0	NASA MEMO 2-9-59E AIR- COOLED TURBINE BLADES WITH TIP CAP FOR IMPROVED LEADING-EDGE COOLING	Next

Bound With Nasa Memo 2-15-59l-2-28-59l

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