[PDF] Effects Of Deflected Thrust On The Longitudinal Aerodynamic Chartacteristics Of A Close Coupled Wing Canard Configuration Download EBook Full (2024)

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Read and Download Long P. Yip book Effects of Deflected Thrust on the Longitudinal Aerodynamic Characteristics of a Close coupled Wing canard Configuration in PDF, EPub, Mobi, Kindle online. Full book Effects of Deflected Thrust on the Longitudinal Aerodynamic Characteristics of a Close coupled Wing canard Configuration. This book was released on 1977 with total page 100 pages. Book excerpt:

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Read and Download Samuel M. Dollyhigh book Static Longitudinal Aerodynamic Characteristics of Close coupled Wing canard Configurations at Mach Numbers from 1 60 to 2 86 in PDF, EPub, Mobi, Kindle online. Full book Static Longitudinal Aerodynamic Characteristics of Close coupled Wing canard Configurations at Mach Numbers from 1 60 to 2 86. This book was released on 1971 with total page 126 pages. Book excerpt: An experimental investigation was made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations. Three canards, ranging in exposed planform area from 17.5 to 30.0 percent of the wing reference area, were employed in this investigation. The canards were either located in the plane of the wing or in a position 18.5 percent of the wing mean geometric chord above the wing plane. Most data obtained were for a model with a 60 deg leading-edge-sweep wing; however, a small amount of data were obtained for a 44 deg leading-edge-sweep wing. The model utilized two balances to isolate interference effects between wing and canard. In general, it was determined that at angle of attack for all configurations investigated with the canard in the plane of the wing an unfavorable interference exists which causes the additional lift on the canard generated by a canard deflection to be lost on the wing due to an increased downwash at the wing from the canard. Further, this interference decreased somewhat with increasing Mach number. Raising the canard above the plane of the wing also greatly decreased the interference of the canard deflection on the wing lift. However, at Mach 2.86 the presence of the canard in the high position had a greater unfavorable interference effect at high angles of attack than the canard in the wing plane. This interference resulted in the in-plane canard having better trimmed performance at Mach 2.86 for the same center-of-gravity location.

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Read and Download Long P. Yip book Effects of Deflected Thrust on the Longitudinal Aerodynamic Chartacteristics of a Close coupled Wing canard Configuration in PDF, EPub, Mobi, Kindle online. Full book Effects of Deflected Thrust on the Longitudinal Aerodynamic Chartacteristics of a Close coupled Wing canard Configuration. This book was released on 1977 with total page 100 pages. Book excerpt: The effects of power on the longitudinal aerodynamic characteristics of a close-coupled wing-canard fighter configuration with partial-span rectangular nozzles at the trailing edge of the wing were investigated. Data were obtained on a basic wing-strake configuration for nozzle and flap deflections from 0 deg to 30 deg and for nominal thrust coefficients from 0 to 0.30. The model was tested over an angle-of-attack range from -2 deg to 40 deg at Mach numbers of 0.15 and 0.18. Results show substantial improvements in lift-curve slope, in maximum lift, and in drag-due-to-lift efficiency when the canard and strakes have been added to the basic wing-fuselage (wing-alone) configuration. Addition of power increased both lift-curve slope and maximum lift, improved longitudinal stability, and reduced drag due to lift on both the wing-canard and wing-canard-strake configurations. These beneficial effects are primarily derived from boundary-layer control due to moderate thrust coefficients which delay flow separation on the nozzle and inboard portion of the wing flaps.

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