{"product_id":"compressible-flow-ii","title":"Compressible Flow II","description":"\u003cp\u003ePart 2 of 3 in the Compressible Flow series. Topics in this product include the theta-beta-M relation and shock polars, Mach reflection, supersonic inlet and nozzle design, shock-expansion theory for supersonic aerofoils, and Prandtl-Meyer expansion theory.\u003c\/p\u003e\u003cp\u003eThis is a 19-page PDF scan of handwritten notes, featuring clickable PDF bookmarks so you can jump straight to any page in a PDF viewer such as Adobe Acrobat. Complete page-by-page contents can be found below so you know exactly what's inside before you buy.\u003c\/p\u003e","brand":"Aeroemilia","offers":[{"title":"Default Title","offer_id":58591184093515,"sku":"AERO-CF2","price":6.0,"currency_code":"GBP","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/1083\/5774\/7019\/files\/compressible-flow-ii-1-cover.jpg?v=1790610371","url":"https:\/\/aeroemilia.com\/products\/compressible-flow-ii","provider":"aeroemilia","version":"1.0","type":"link"}