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Effects Of Deflected Wing Tips On The Aero Dynamic Characteristics Of A Canard Configuration At Mach Numbers From 07 To 35
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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:
Book Synopsis Effects of Deflected Wing Tips on the Aero- Dynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 by :
Download or read book Effects of Deflected Wing Tips on the Aero- Dynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 written by and published by . This book was released on 1960 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Interference Effects of Canard Controls on the Longitudinal Aerodynamic Characteristics of a Winged Body at Mach 10 by : Cuyler W. Brooks (Jr.)
Download or read book Interference Effects of Canard Controls on the Longitudinal Aerodynamic Characteristics of a Winged Body at Mach 10 written by Cuyler W. Brooks (Jr.) and published by . This book was released on 1968 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Canard Planform and Wing-leading-edge Modification on Low-speed Longitudinal Aerodynamic Characteristics of a Canard Airplane Configuration by : Bernard Spencer
Download or read book Effects of Canard Planform and Wing-leading-edge Modification on Low-speed Longitudinal Aerodynamic Characteristics of a Canard Airplane Configuration written by Bernard Spencer and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted at low subsonic speeds to study the effects of canard planform and wing-leading-edge modification on the longitudinal aerodynamic characteristics of a general research canard airplane configuration. The basic wing of the model had a trapezoidal planform, an aspect ratio of 3.0, a taper ratio of 0.143, and an unswept 80-percent-chord line. Modifications to the wing included addition of full-span and partial-span leading-edge chord-extensions. Two canard planforms were employed in the study one was a 60° sweptback delta planform and the other was a trapezoidal planform similar to that of the basic wing. Modifications to these canards included addition of a full-span leading-edge chord-extension to the trapezoidal planform and a fence to the delta planform. For the basic-wing-trapezoidal-canard configuration, rather abrupt increases in stability occurred at about 12° angle of attack. A slight pitch-up tendency occurred for the delta-canard configuration at approximately 8° angle of attack. A comparison of the longitudinal control effectiveness for the basic-wing-trapezoidal-canard combination and for the basic-wing-delta-canard combination indicates higher values of control effectiveness at low angles of attack for the trapezoidal canard. The control effectiveness for the delta-canard configuration, however, is seen to hold up for higher canard deflections and to higher angles of attack. Use of a full-span chord-extension deflected approximately 30° on the trapezoidal canard greatly improved the control characteristics of this configuration and enabled a sizeable increase in trim lift to be realized.
Book Synopsis Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing by :
Download or read book Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing written by and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of the Close-Coupled Canard as Applied to Low-to-Moderate Swept Wings. Volume 3. Transonic-Supersonic Speed Regime by : David W. Lacey
Download or read book Aerodynamic Characteristics of the Close-Coupled Canard as Applied to Low-to-Moderate Swept Wings. Volume 3. Transonic-Supersonic Speed Regime written by David W. Lacey and published by . This book was released on 1979 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis of the effects of canard shape, position, and deflection on the aerodynamic characteristics of two general research models having leading edge sweep angles of 25 and 50 degrees is presented. The analysis summarizes findings of three experimental transonic wind-tunnel programs and one supersonic wind-tunnel program conducted at this Center between 1970 and 1974. The analysis is based on four canard geometries varying in planform from a 60-degree delta to a 25-degree swept wing, high aspect ratio canard. The canards were tested at several positions and deflected from -10 to +10 degrees. In addition, configurations consisting of a horizontal tail and a canard with horizontal tails are analyzed. Results of the analysis indicate that the canard is effective in increasing lift and decreasing drag at Mach numbers from subsonic to high transonic speeds by delaying wing separation. The effectiveness of the canard is, however, decreased with increasing Mach number. At supersonic speeds the canard has little or no favorable effects on lift or drag. It is further shown that the horizontal tail is a superior trimming device than the close- coupled canard at low-to-moderate angles of attack and that a configuration consisting of canard, wing, and horizontal tail is superior in performance, to either canard or horizontal tail at high angles of attack.
Book Synopsis An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-mounted Canard Configurations at Transonic Mach Numbers by : James R Burt (Jr.)
Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-mounted Canard Configurations at Transonic Mach Numbers written by James R Burt (Jr.) and published by . This book was released on 1974 with total page 778 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted at the CALSPAN Corporation's transonic wind tunnel to determine the aerodynamic characteristics of several nose-mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. Angle of attack was varied from -3 to 12 degrees and Mach number was varied from 0.6 to 1.25. Aerodynamic loads were measured separately for each of the four canards and tail surfaces, and the total model.
Book Synopsis Effects of Deflected Thrust on the Longitudinal Aerodynamic Chartacteristics of a Close-coupled Wing-canard Configuration by : Long P. Yip
Download or read book Effects of Deflected Thrust on the Longitudinal Aerodynamic Chartacteristics of a Close-coupled Wing-canard Configuration written by Long P. Yip and published by . This book was released on 1977 with total page 100 pages. Available in PDF, EPUB and Kindle. 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.
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 Thrust on the Longitudinal Aerodynamic Characteristics of a Close-coupled Wing-canard Configuration by : Long P. Yip
Download or read book Effects of Deflected Thrust on the Longitudinal Aerodynamic Characteristics of a Close-coupled Wing-canard Configuration written by Long P. Yip and published by . This book was released on 1977 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90° by : Gerald V. Foster
Download or read book Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90° written by Gerald V. Foster and published by . This book was released on 1961 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight written by and published by . This book was released on 1960 with total page 38 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:
Book Synopsis Effect of Canard Location and Size on Canard-wing Interference and Aerodynamic-center Shift Related to Maneuvering Aircraft at Transonic Speeds by : Blair B. Gloss
Download or read book Effect of Canard Location and Size on Canard-wing Interference and Aerodynamic-center Shift Related to Maneuvering Aircraft at Transonic Speeds written by Blair B. Gloss and published by . This book was released on 1974 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Canard and Vertical Tails on the Aerodynamic Characteristics of a Model with a 59 ̊sweptback Wing at a Mach Number of 0.30 by : William P. Henderson
Download or read book The Effect of Canard and Vertical Tails on the Aerodynamic Characteristics of a Model with a 59 ̊sweptback Wing at a Mach Number of 0.30 written by William P. Henderson and published by . This book was released on 1974 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63 by : Maurice O. Feryn
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63 written by Maurice O. Feryn and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Some Wing Variations Including Wingtip Deflection on the Static Longitudinal Aerodynamic Characteristics of a Delta-wing Configuration at Supersonic Speeds by :
Download or read book Effects of Some Wing Variations Including Wingtip Deflection on the Static Longitudinal Aerodynamic Characteristics of a Delta-wing Configuration at Supersonic Speeds written by and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
