{"version":"1.0","type":"rich","provider_name":"EbookNetworking","provider_url":"https://www.ebooknetworking.net","title":"Wind tunnel tests at mach numbers up to 1, 8 on a model with 1, 36 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188) (Current papers; no.798)","author_name":"Aeronautical Research Council","thumbnail_url":"https://www.ebooknetworking.net/books/noimage.jpg","thumbnail_width":330,"thumbnail_height":500,"html":"<a href=\"https://www.ebooknetworking.net/books_detail-B0000CMKZ2.html\">Wind tunnel tests at mach numbers up to 1, 8 on a model with 1, 36 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188) (Current papers; no.798)</a>","width":400,"height":300}