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Static Longitudinal Aerodynamic Characteristics Of An Elastic Canard Fuselage Configuration As Measured In Air And In Freon 12 At Mach Numbers Up To 092
Download Static Longitudinal Aerodynamic Characteristics Of An Elastic Canard Fuselage Configuration As Measured In Air And In Freon 12 At Mach Numbers Up To 092 full books in PDF, epub, and Kindle. Read online Static Longitudinal Aerodynamic Characteristics Of An Elastic Canard Fuselage Configuration As Measured In Air And In Freon 12 At Mach Numbers Up To 092 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Static Longitudinal Aerodynamic Characteristics of an Elastic Canard-fuselage Configuration as Measured in Air and in Freon-12 at Mach Numbers Up to 0.92 by : Edward Carson Yates
Download or read book Static Longitudinal Aerodynamic Characteristics of an Elastic Canard-fuselage Configuration as Measured in Air and in Freon-12 at Mach Numbers Up to 0.92 written by Edward Carson Yates and published by . This book was released on 1963 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 to 2.86 by : Samuel M. Dollyhigh
Download or read book Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 to 2.86 written by Samuel M. Dollyhigh and published by . This book was released on 1971 with total page 126 pages. Available in PDF, EPUB and Kindle. 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.
Book Synopsis Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards by : A. Warner Robins
Download or read book Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards written by A. Warner Robins and published by . This book was released on 1979 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book ASME Technical Papers written by and published by . This book was released on with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Paper written by and published by . This book was released on 1993 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds by : Paul G. Fournier
Download or read book Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds written by Paul G. Fournier and published by . This book was released on 1961 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 To.2.86 by : Samuel M. Dollyhigh
Download or read book Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 To.2.86 written by Samuel M. Dollyhigh and published by . This book was released on 1971 with total page 115 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been 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° leading-edge-sweep wing; however, a small amount of data were obtained for a 44° 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.--P. [i].
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails by : Victor L. Peterson
Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails written by Victor L. Peterson and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 by : Victor L. Peterson
Download or read book Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 written by Victor L. Peterson and published by . This book was released on 1960 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of Aircraft written by and published by . This book was released on 1999 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Longitudinal Aerodynamic Characteristics of a 1/30-scale Canard- Airplane Model Having a Wing with an Aspect Ratio of 6.0 by :
Download or read book Subsonic Longitudinal Aerodynamic Characteristics of a 1/30-scale Canard- Airplane Model Having a Wing with an Aspect Ratio of 6.0 written by and published by . This book was released on 1962 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.50 of a Canard Configuration Having Varied Body Shapes by : Donald T. Gregory
Download or read book Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.50 of a Canard Configuration Having Varied Body Shapes written by Donald T. Gregory and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Canard Relative Size and Vertical Location on the Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics for a Model with a Swept Forward Wing by : Jarrett K. Huffman
Download or read book The Effect of Canard Relative Size and Vertical Location on the Subsonic Longitudinal and Lateral-directional Static Aerodynamic Characteristics for a Model with a Swept Forward Wing written by Jarrett K. Huffman and published by . This book was released on 1979 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Unswept Canard by : Victor L. Peterson
Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Unswept Canard written by Victor L. Peterson and published by . This book was released on 1958 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration are presented without analysis for the Mach number range from 0.70 to 2.22. The configuration consisted of an aspect ratio vertical tail, and a Sears-Haack body. The hinge line of the canard was in the extended chord plane of the wing, 1.15 wing mean aerodynamic chords ahead of the reference center of moments. The ratio of the area of the exposed canard panels to the total area of the wing is 8.1 percent. Data are presented for various combinations of the canard, wing, and vertical tail for an angle-of-attack range from -6 to 18 degrees. The canard deflection angles ranged from 0 to 20 degrees.
Book Synopsis Low-speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing-edge Flap Controls in Combination by : Bernard Spencer
Download or read book Low-speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing-edge Flap Controls in Combination written by Bernard Spencer and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration written by and published by . This book was released on 1962 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
