Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.]

• Material Type: 図書
• Title: Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.]
• Series Title: NASA/TM ; 1999-209701
• Title Heading: NASA technical memorandum ; 209701
• Author Heading: Campbell, Bryan A; Langley Research Center
• Publication Date (W3CDTF): 1999
• Extent: microfiche
• Size: 11 × 15 cm
• Alternative Title: Subsonic investigation of leading edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration
• Place of Publication (Country Code): US
• Text Language Code: eng
• Note (Material Type): [microform]
• Subject Heading: Subsonic wind tunnels; Leading edge flaps; Vortices; Supersonic transports; Aerodynamic configurations; Separated flow
• Note (General): Shipping list no.: 2000-0596-M; Physical description for original version: 1 v
• Note (Original Version): 原資料の出版事項: Hampton, Va. ; Hanover, MD ; Springfield, VA : National Aeronautics and Space Administration, Langley Research Center : Available from NASA Center for Aerospace Information : National Technical Information Service [distributor, 1999]; SUPTDOC番号: NAS 1.15: 209701; GPO管理番号: 0830-D (MF)
• Holding library: 国立国会図書館
• Call No.: YCA-NAS 1.15:209701
• Data Provider (Database): 国立国会図書館 : 国立国会図書館蔵書; https://ndlsearch.ndl.go.jp
• Bibliographic ID (NDL): 000006632776; http://id.ndl.go.jp/bib/000006632776
• OCLC No.: 44120738; https://www.worldcat.org/oclc/44120738
• Bibliographic Record Category (NDL): 281