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Thermal-structural analyses of Space Shuttle Main Engine (SSME) hot section components [PDF]

open access: yes
Three dimensional nonlinear finite element heat transfer and structural analyses were performed for the first stage high pressure fuel turbopump (HPFTP) blade of the space shuttle main engine (SSME).
Abdul-Aziz, Ali, Thompson, Robert L.
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SR-7A aeroelastic model design report [PDF]

open access: yes
A scale model was designed to simulate the aeroelastic characteristics and performance of the 2.74 meter (9 ft.) diameter SR-7L blade. The procedures used in this model blade design are discussed.
Auyeung, S., Nagle, D., Turnberg, J.
core   +1 more source

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