Normal view MARC view ISBD view

SUMMARY OF DESIGN AND BLADE-ELEMENT PERFORMANCE DATA FOR 12 AXIAL-FLOW PUMP ROTOR CONFIGURATIONS.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1973Description: 214.DDC classification: NASA | TN D-7074

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-7074 (Browse shelf)	Not for loan		TR12201

Total holds: 0

Previous								Next
Previous	NASA TN D-7071 LOW-SPEED AERODYNAMIC CHARACTERISTICS OF AN AIRFOIL OPTIMIZED FOR MAXIMUM LIFT COEFFICIENT.	NASA TN D-7072 EFFECTS OF FUEL NOZZLE DESIGN ON PERFORMANCE OF AN EXPERIMENTAL ANNULAR COMBUSTOR USING NATURAL GAS FUEL.	NASA TN D-7073 FRETTING OF SECONDARY-SEAL-RING CANDIDATE MATERIALS IN AIR AT TEMPERATURES TO 816 DEGREE C.	NASA TN D-7074 SUMMARY OF DESIGN AND BLADE-ELEMENT PERFORMANCE DATA FOR 12 AXIAL-FLOW PUMP ROTOR CONFIGURATIONS.	NASA TN D-7075 NOIS GENERATED BY IMPINGEMENT OF A JET UPON A LARGE FLAT BOARD.	NASA TN D-7076 EFFECTS OF INSTALLATION CAUSED FLOW DISTORTION ON NOISE FROM A FAN TURBOFAN ENGINES.	NASA TN D-7077 DISSOCIATION RATE OF BROMINE DIATOMICS IN AN ARGON HEAT BATH.	Next

Bound With Nasa Tn D-7070-73, 7075-79

There are no comments for this item.

PKK Library