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ANALYSIS OF GEOMETRY AND DESIGN POINT PERFORMENCE OF AXIAL FLOW TURBINES [NASA CR-1181] : I - deveopment of the analysis method and the loss coefficient correlation

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Material type: Text

TextLanguage: English Series: National Aeronutics and Space Administration (NASA)Publication details: NASA, WASHINGTON, D.C.Description: vii,107pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-1181 (Browse shelf(Opens below))	Not for loan		101452

Total holds: 0

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Previous	NACA TN-2882 Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system	NACA TN-2883 Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-alloy Hand Forgings	NACA TN-2886 An analysis of statically indeterminate trusses having members stressed beyond the proportional limit	NASA CR-1181 ANALYSIS OF GEOMETRY AND DESIGN POINT PERFORMENCE OF AXIAL FLOW TURBINES [NASA CR-1181]	NASA CR-1182 AN INVESTIGATION OF THIN FILM OXYGEN PARTIAL PRESSURE SENSORS [NASA CR-1182]	NASA CR-1183 PREPROCESSING ELECTRONIC SATELLITE OBSERVATIONS [NASA CR-1183]	NASA CR-1184 OXIDATION RESISTANT MATERIALS FOR TRANSPIRATION COOLED GAS TURBINE BLADES [NASA CR 1184]	Next

Bound with NASA CR-1181-85 (Bound Acc no. 101542)

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