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PERFORMANCE EVALUATION OF A TWO-STAGE AXIAL-FLOW TURBINE FOR TWO VALUES OF TIP CLEARANCE

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BookPublisher: Nasa, Washington, D.C. Description: 19.DDC classification: NASA | TN D-4388

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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-4388 (Browse shelf)	Not for loan		TR15092

Total holds: 0

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Previous	NASA TN D-4385 CORRELATION OF TRANSIENT SPECTRA WITH PERFORMANCE IN COAXIAL PLASMA GUNS	NASA TN D-4386 PARAMETRIC MASS ANALYSIS AND COMPARISON OF TWO TYPES OF REACTANT COOLING-AND-STORAGE UNITS FOR A LUNAR-BASED HYDROGEN-OXYGEN REGENERATIVE FUEL-CELL SYSTEM	NASA TN D-4387 VENTURI SCALING STUDIES ON THERMODYNAMIC EFFECTS OF DEVELOPED CAVITATION OF FREON-114	NASA TN D-4388 PERFORMANCE EVALUATION OF A TWO-STAGE AXIAL-FLOW TURBINE FOR TWO VALUES OF TIP CLEARANCE	NASA TN D-4389 COLD-AIR INVESTIGATION OF A TURBINE FOR HIGH-TEMPERATURE-ENGINE APPLICATION	NASA TN D-439 AXIAL-LOAD FATIGUE TESTS ON 17-7 PH STAINLESS STEEL UNDER CONSTANT-AMPLITUDE LOADING.	NASA TN D-4390 APPLICATION OF DIRECTIONAL SOLIDIFICATION TO A NASA NICKEL-BASE ALLOY (TAZ-8B)	Next

Bound With Nasa Tn D-4381-87,4389-90

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