Thermal and structural analysis of a hollow core Space Shuttle Main Engine (SSME) turbine blade
By: Ali Abdul-Aziz and Sreeramesh Kalluri, Michael A. McGaw.
Contributors: Kalluri, Sreeramesh.; McGaw, Michael A.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107089.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Crystal structure.; Finite element method.; Heat resistant alloys.; Heat transfer.; Nickel alloys.; Single crystals.; Space Shuttle main engine.; Stress distribution.; Structural analysis.; Turbine blades.; Turbine pumps.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0493-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 1 microfiche.