Normal view MARC view ISBD view

COLD-AIR INVESTIGATION OF A TURBINE FOR HIGH-TEMPERATURE-ENGINE APPLICATION

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. Description: 22.DDC classification: NASA | TN D-4389

average rating: 0.0 (0 votes)

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-4389 (Browse shelf)	Not for loan		TR15093

Total holds: 0

Previous								Next
Previous	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)	NASA TN D-4392 - COLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN-OXYGEN ROCKET ENGINE	Next

Bound With Nasa Tn D-4381-88,4390

There are no comments for this item.

PKK Library