In this Technical Brief we illustrate the efficacy of the Robust Concept Exploration Method as applied to the preliminary design of a turbine lift engine for Advanced Short Take-Off and Vertical Landing (ASTOVL) fighter aircraft. This example is defined in collaboration with the Rolls-Royce Atlanta Engineering Group.
Facilitating Concept Exploration for Configuring Turbine Propulsion Systems
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Koch, P. N., Allen, J. K., Mistree, F., and Barlow, A. (December 1, 1998). "Facilitating Concept Exploration for Configuring Turbine Propulsion Systems." ASME. J. Mech. Des. December 1998; 120(4): 702–706. https://doi.org/10.1115/1.2829334
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