登入選單
返回Google圖書搜尋
High-temperature Nozzle-throat Heat Transfer and Thermal Protection for Hypersonic Shock Tunnels: Analytic studies
出版Cornell Aeronautical Laboratory, Incorporated, 1964
URLhttp://books.google.com.hk/books?id=eYz-GwAACAAJ&hl=&source=gbs_api