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EXPERIMENTAL INVESTIGATION OF ADVANCED CONCEPTS TO INCREASE TURBINE BLADE LOADING : I. ANALYSIS AND DESIGN

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BookPublisher: Nasa, Washington, D.C. 1967Description: viii,151.DDC classification: NASA | CR-735 -

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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-735 - (Browse shelf)	Not for loan		TR8692

Total holds: 0

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Previous	NASA CR-732 - STEADY-STATE AND DYNAMIC PROPERTIES OF JOURNAL BEARINGS IN LAMINAR AND SUPERLAMINAR FLOW REGIMES	NASA CR-733 - Steady-state and dynamic properties of journal bearings in laminar and superlaminar flow regimes	NASA CR-734 - FLUID AMPLIFIER STATE-OF-THE-ART REPORT	NASA CR-735 - EXPERIMENTAL INVESTIGATION OF ADVANCED CONCEPTS TO INCREASE TURBINE BLADE LOADING	NASA CR-737 - AERODYNAMIC CHARACTERISTICS FOR CONE-CYLINDER-FRUSTUM-CYLINDER CONFIGURATIONS AT MACH NUMBERS FROM 0.7 TO 1.96	NASA CR-738 - STUDY OF METHODS FOR SYNCHRONIZING REMOTELY-LOCATED CLOCKS	NASA CR-739 - BIO-THERMAL RESPONSES TO VARIED WORK PROGRAMS IN MEN KEPT THERMALLY NEUTRAL BY WATER COOLED CLOTHING	Next

Bound With Nasa Cr-731-35

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