Normal view MARC view ISBD view

METHOD FOR CALCULATING ALLOWABLE CREEP STRESS IN LINEARLY INCREASING STRESS ENVIRONMENT.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1970Description: 9.DDC classification: NASA | TN D-4352

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-4352 (Browse shelf)	Not for loan		TR11543

Total holds: 0

Previous								Next
Previous	NASA TN D-4340 EFFECTS OF WALL PRESSURE DISTRIBUTION AND LIQUID TEMPERATURE ON INCIPIENT CAVITATION OF FREON-114 AND WATER IN VENTURI FLOW	NASA TN D-4347 DEVELOPMENT AND APPLICATION OF A LOCAL LINEARIZATION ALGORAITHM FOR THE INTGERIZATION OF QUATERNION RATE EQUATIONS IN REAL-TIME FLIGHT SIMULATION PROBLEMS.	NASA TN D-435 TRANSONIC AND SUPERSONIC WIND-TUNNEL TESTS OF WING-BODY COMBINATIONS DESIGNED FOR HIGH EFFICIENCY AT A MACH NUMBER OF 1.41	NASA TN D-4352 METHOD FOR CALCULATING ALLOWABLE CREEP STRESS IN LINEARLY INCREASING STRESS ENVIRONMENT.	NASA TN D-4353 TRANSIENT SOLIDFICATION OF A FLOWING LIQUID A COLD PLATE INCLUDING HEAT CAPACITIES OF FROZEN LAYER AND PLATE.	NASA TN D-4354 AN UNCERTAINTY ANALYSIS FOR SATELLITE CALORIMETRIC MEASUREMENTS.	NASA TN D-4355 FRICTION TORQUE OF BALL BEARINGS IN VACUUM WITH SEVEN POLYTERAFLUOROETHYLENE- COMPOSITION.	Next

Bound With Nasa Tn D-4351,4353-60.

There are no comments for this item.

PKK Library