Effect of Nacelles on Aerodynamic Characteristics of an Executive-jet Model with Simulated, Partial-chord, Laminar-flow-control Wing GloveNational Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982 - Aerodynamics, Transonic - 101 pages |
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Effect of Nacelles on Aerodynamic Characteristics of an Executive-jet Model ... Richard Lawson Campbell No preview available - 1982 |
Common terms and phrases
10-Foot Tunnel Aeronautics and Space aft of nose airfoil angle of attack boundary layer compressibility drag Concluded constant angle Continued drag coefficient Effect of horizontal Effect of nacelles executive jet EXECUTIVE-JET MODEL Figure 16 Figure 20 Figure 9 forward portion fuselage glove design glove region horizontal tail increment in drag Laminar Flow Laminar Flow Control Langley High-Speed Langley Research Center leading edge longitudinal aerodynamic characteristics loss in lift mean aerodynamic chord NACA nacelles caused nacelles on wing nacelles-off and nacelles-on NASA National Aeronautics negative pressure coefficients number and angle numbers from 0.40 outboard partial-chord pressure orifice installation range of Mach Space Administration suction tail on wing Tests were conducted transonic U.S. Customary Units Wing oil-flow photographs wing panel wing pressure distributions x/c z/c x/c z/c x/c z/c ОО Ө Ө Ср ბი کی می るる