{ "item_title" : "System Study for Axial Vane Engine Technology", "item_author" : [" Nasa Technical Reports Server (Ntrs)", "Et Al", "Patrick R. Badley "], "item_description" : "The purpose of this engine feasibility study was to determine the benefits that can be achieved by incorporating positive displacement axial vane compression and expansion stages into high bypass turbofan engines. These positive-displacement stages would replace some or all of the conventional compressor and turbine stages in the turbine engine, but not the fan. The study considered combustion occurring internal to an axial vane component (i.e., Diesel engine replacing the standard turbine engine combustor, burner, and turbine); and external continuous flow combustion with an axial vane compressor and an axial vane turbine replacing conventional compressor and turbine systems.", "item_img_path" : "https://covers1.booksamillion.com/covers/bam/1/28/723/610/1287236103_b.jpg", "price_data" : { "retail_price" : "18.75", "online_price" : "18.75", "our_price" : "18.75", "club_price" : "18.75", "savings_pct" : "0", "savings_amt" : "0.00", "club_savings_pct" : "0", "club_savings_amt" : "0.00", "discount_pct" : "10", "store_price" : "" } }

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