02137cam a2200409 a 4500100393401MiAaHDL20250726000000.0m d cr bn ---auaua131003s1954 dcua b f000 0 eng d(MiU)990131340900106381sdr-miu.990131340900106381(MiU)MIU01000000000000013134090-goog(OCoLC)859343532(MiU)Aleph013134090NACARengNACAROCLCOOCLCQOCLCOOCLCFOCLCQOCLCOUtOrBLWEYMGY 3.N21/5:15/L54D09aFischetti, Thomas L.Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60° sweptback-wing--indented-body configuration at transonic speeds /by Thomas L. Fischetti.Washington, D.C. :National Advisory Committee for Aeronautics,1954.17 pages :illustrations ;27 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierNACA research memorandum ;L54D09a"June 17, 1954."Includes bibliographical references (page 9).Mode of access: Internet.Stability of airplanes, Longitudinal.fasthttp://id.worldcat.org/fast/1131217Aerodynamics, Transonic.fasthttp://id.worldcat.org/fast/798229Aerodynamics, Transonic.http://id.loc.gov/authorities/subjects/sh85001299AirplanesWings, Swept-backStability.Stability of airplanes, Longitudinal.http://id.loc.gov/authorities/subjects/sh85127188United States.National Adviosry Committee for Aeronautics.NACA research memorandum.Langley Aeronautical Laboratory.http://id.loc.gov/authorities/names/n81018841http://id.loc.gov/rwo/agents/n81018841Technical Report Archive & Image Library (TRAIL)3901508650696410039340120241218072128.020250726000000.020260302165435.02026-04-01T17:52:29Z2026-04-01T17:30:03ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.990131340900106381MiUSDRGWLA013134090mdp.39015086506964MIU990131340900106381MIUGWLA20260401googlemdp.390150865069641954pdbibUS fed doc