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Cold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factory of 4 designed for an integral lift engine : I - Turbine design and performance of first stage

Cold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factory of 4 designed for an integral lift engine : I - Turbine design and performance of first stage - - Washington, D.C. National Aeroronautic and Space Administration (NASA) 1975 - 38 p. - NASA TN D 3289 : 1975 .

ISBN:

Subjects--Topical Terms:

Turbine aerodynamics, High stage loading, Fan drive turbines

Universal Decimal Class. No.: LNASA TN D 3289 : 1975

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