Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
The Effect Of Aileron Span And Spanwise Location On The Low Speed Lateral Control Characteristics On An Untapered Wing Of Aspect Ratio 209 And 45 Degrees Sweepback
Download The Effect Of Aileron Span And Spanwise Location On The Low Speed Lateral Control Characteristics On An Untapered Wing Of Aspect Ratio 209 And 45 Degrees Sweepback full books in PDF, epub, and Kindle. Read online The Effect Of Aileron Span And Spanwise Location On The Low Speed Lateral Control Characteristics On An Untapered Wing Of Aspect Ratio 209 And 45 Degrees Sweepback ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis The Effect of Aileron Span and Spanwise Location on the Low-speed Lateral Control Characteristics on an Untapered Wing of Aspect Ratio 2.09 and 45 Degrees Sweepback by : Rodger L. Naeseth
Download or read book The Effect of Aileron Span and Spanwise Location on the Low-speed Lateral Control Characteristics on an Untapered Wing of Aspect Ratio 2.09 and 45 Degrees Sweepback written by Rodger L. Naeseth and published by . This book was released on 1950 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Aspect Ratio and Sweepback on the Low-speed Lateral Control Characteristics of Untapered Low-aspect-ratio Wings Equipped with Retractable Ailerons by : Jack Fischel
Download or read book Effect of Aspect Ratio and Sweepback on the Low-speed Lateral Control Characteristics of Untapered Low-aspect-ratio Wings Equipped with Retractable Ailerons written by Jack Fischel and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results and discussion are presented of a low-speed lateral-control investigation of three untapered unswept wings of aspect ratio 1.13, 2.13, and 4.13 and an untapered 45 degrees sweptback wing of aspect ratio 2.09 equipped with 0.60-semispan retractable ailerons having various projections. Continuous-span ailerons were tested at outboard stations on the unswept wings, and plain (continuous span) and stepped (segmented) ailerons were tested at various spanwise stations with and without simulated actuating arms on the sweptback wing.
Book Synopsis Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Unswept Untapered Low-aspect-ratio Wings by : Rodger L. Naeseth
Download or read book Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Unswept Untapered Low-aspect-ratio Wings written by Rodger L. Naeseth and published by . This book was released on 1951 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of untapered, unswept, complete wings of apsect ratios 1.13, 2.13, 4.13, and 6.13 was investigated at a Mach number of 0.26 to determine the effect of aspect ratio on the lateral control characteristics of the wings equipped with 0.25-chord sealed ailerons of various spans and of various spanwise locations. Design charts are presented for computing aileron effectiveness of low-aspect-ratio, untapered, unswept wings. Experimental values of control effectivenesss are compared with values estimated by theoretical methods.
Book Synopsis Effect of Aspect Ratic and Sweepback on the Low-Speed Lateral Control Characteristics of Untapered Low-Aspect-Ratio Wings Equipped With Retractable Ailerons by :
Download or read book Effect of Aspect Ratic and Sweepback on the Low-Speed Lateral Control Characteristics of Untapered Low-Aspect-Ratio Wings Equipped With Retractable Ailerons written by and published by . This book was released on 1951 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: A low-speed wind-tunnel investigation was made to determine the lateral control characteristics of three untapered unswept wings of aspect ratio 1.13, 2.13, and 4.13 and an untapered 4%o sweptback wing of aspect ratio 2.09 equipped with O.60-semispan retractable ailerons having various projections. Each of the wings had an NACA 64A010 airfoil section and had the ailerons mounted at the 0. 70-chord station. The continuous- span aileron investigated on the unswept wings spanned the outboard stations of each wing; whereas the plain (continuous span) and stepped (segmented) retractable ailerons investigated on the sweptback wing were located at various spanwise stations and were tested with and without simulated actuating arms.
Book Synopsis Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio by : Edward J. Hopkins
Download or read book Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio written by Edward J. Hopkins and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0, 35, and 45 degrees. The wing span was decreased to give aspect ratios 6.8, 5.3, 4.2, 3.4, and 2.8. The effects of independent variations of sweep and aspect ratio on the lift, pitching-moment, and span-load characteristics of the wings are compared with the effects estimated by use of the Weissinger method.
Book Synopsis Investigation of Effect of Span and Spanwise Location of Plain and Stepped Spoiler Ailerons on Lateral Control Characteristics of a Wing with Leading Edge Swept Back 51.3 Degrees by : Jack Fischel
Download or read book Investigation of Effect of Span and Spanwise Location of Plain and Stepped Spoiler Ailerons on Lateral Control Characteristics of a Wing with Leading Edge Swept Back 51.3 Degrees written by Jack Fischel and published by . This book was released on 1950 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation was made at low speed to determine the lateral control characteristics of a 51.3 degrees sweptback-wing model equipped with either plain or stepped spoiler ailerons having a fixed projection of 5-percent-wing chord and various spans and spanwise locations. The spoiler-aileron configurations were tested on the wing alone, on the wing with a simulated fuselage, on the wing with a simulated fuselage and either a 0.487-span outboard drooped nose, a 0.487-span inboard split flap, or a combination of the two devices.
Book Synopsis A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps by : Powell M. Lovell
Download or read book A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps written by Powell M. Lovell and published by . This book was released on 1950 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight-tunnel investigation has been made to compare the dynamic lateral control characteristics provided by step plug ailerons on a sweptback-wing model having full-span flaps. The model had a 38 degree sweptback wing with an aspect ratio of 3 and a taper ratio of 0.05. The static stability and control characteristics of the flight-test model were determined from force tests and the time-lag characteristics of the ailerons were determined from stand tests in which there was freedom only in roll. Flight tests of the model were made over a range of lift coefficient from 1.0 through the stall.
Book Synopsis Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Untapered Low-aspect-ratio Wings Equipped with Flap and with Retractable Ailerons by : Jack Fischel
Download or read book Effect of Aspect Ratio on the Low-speed Lateral Control Characteristics of Untapered Low-aspect-ratio Wings Equipped with Flap and with Retractable Ailerons written by Jack Fischel and published by . This book was released on 1952 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing by : Donald E. Hewes
Download or read book The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing written by Donald E. Hewes and published by . This book was released on 1951 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.
Book Synopsis Low-speed Lateral Stability and Aileron-effectiveness Characteristics at a Reynolds Number of 3.5 X (10)6 of a Wing with Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip by : Roy H. Lange
Download or read book Low-speed Lateral Stability and Aileron-effectiveness Characteristics at a Reynolds Number of 3.5 X (10)6 of a Wing with Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip written by Roy H. Lange and published by . This book was released on 1950 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of End Plates on Swept Wings at Low Speed by : John M. Riebe
Download or read book The Effect of End Plates on Swept Wings at Low Speed written by John M. Riebe and published by . This book was released on 1950 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 300 mph 7- by 10-foot tunnel to determine the effects of various sizes and shapes of end plates on the aileron characteristics and on the aerodynamic characteristics in pitch and yaw of a wing of aspect ratio 2, no taper, and a sweepback of 45 degrees and a wing of aspect ration 4, taper ratio 0.6, and a sweepback of 46.7 degrees. Free-roll characteristics were obtained with two end-plate configurations on a wing aspect ratio 3, taper ratio 0.6, and a sweepback of 35 degrees in order to determine the effect of end plates on wing damping in roll.
Book Synopsis Effects of Finite Span on the Section Characteristics of Two 45 Degree Sweptback Wings of Aspect Ratio 6 by : Lynn W. Hunton
Download or read book Effects of Finite Span on the Section Characteristics of Two 45 Degree Sweptback Wings of Aspect Ratio 6 written by Lynn W. Hunton and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the finite-span effects on the local loading characteristics of two sweptback wings at low speed has been made with a view toward providing some insight into the usefulness of two-dimensional section data and span-loading theory for determining the characteristics of sections of a swept wing. The two wings considered, for which complete pressure-distribution data were available at large scale, were identical in plan form having 45 degrees of sweepback and an aspect ratio of 6 and differed in twist in sections, the latter being the NACA 64A010 and NACA 64A810.
Book Synopsis Lateral Control Characteristics of Two Structural Similar Flexible Wings with 45 Degrees Sweep: a Sweptback Wing and a Wing with M Plan Form by : Rodger L. Naeseth
Download or read book Lateral Control Characteristics of Two Structural Similar Flexible Wings with 45 Degrees Sweep: a Sweptback Wing and a Wing with M Plan Form written by Rodger L. Naeseth and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A low-speed wind-tunnel investigation was made to determine the static lateral control characteristics of flap-type and retractable spoiler-type ailerons on a rigid sweptback wing, a flexible sweptback wing, and a flexible M-wing. A few tests were also made with a half-delta tip control on the flexible sweptback wing. The semispan wing models were of aspect ratio 6.0, taper ratio of 0.6, and had NACA 65A009 airfoil sections parallel to the free-stream direction. The quarter-chord lines of the wings were swept 45 degrees and the break in the M-wing was at the half semispan location.
Book Synopsis Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Degree and 45 Degree Sweptback Wings of Aspect Ratio 6 by : William D. Morrison
Download or read book Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Degree and 45 Degree Sweptback Wings of Aspect Ratio 6 written by William D. Morrison and published by . This book was released on 1951 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: An aerodynamic investigation has been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of taper-in-thickness on the aerodynamics characteristics of wings having 35 and 45 degrees of sweep-back, aspect ratio 6, and taper ratio 0.60. The wings were tapered from NACA 65A009 airfoil sections at the root chord to NACA 65A003 airfoil sections at the tip chord. The test Mach number range was from 0.60 to 1.14 at a Reynolds number of the order of 500,000.
Book Synopsis Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron by : Jack F. Runckel
Download or read book Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron written by Jack F. Runckel and published by . This book was released on 1961 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings with 0 Degrees and 45 Degrees Sweep at Subsonic, Transonic and Supersoni Speedsc by : H. Kurt Strass
Download or read book The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings with 0 Degrees and 45 Degrees Sweep at Subsonic, Transonic and Supersoni Speedsc written by H. Kurt Strass and published by . This book was released on 1950 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
