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Investigation Of Low Speed Lateral Control And Hinge Moment Characteristics Of A 20 Percent Chord Plain Aileron On A 477 Sweptback Wing Of Aspect Ratio 51 At A Reynolds Number Of 60 X 106
Download Investigation Of Low Speed Lateral Control And Hinge Moment Characteristics Of A 20 Percent Chord Plain Aileron On A 477 Sweptback Wing Of Aspect Ratio 51 At A Reynolds Number Of 60 X 106 full books in PDF, epub, and Kindle. Read online Investigation Of Low Speed Lateral Control And Hinge Moment Characteristics Of A 20 Percent Chord Plain Aileron On A 477 Sweptback Wing Of Aspect Ratio 51 At A Reynolds Number Of 60 X 106 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Investigation of Low-speed Lateral Control and Hinge-moment Characteristics of a 20-percent-chord Plain Aileron on a 47.7 Sweptback Wing of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X (10)6 by : William M. Hadaway
Download or read book Investigation of Low-speed Lateral Control and Hinge-moment Characteristics of a 20-percent-chord Plain Aileron on a 47.7 Sweptback Wing of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X (10)6 written by William M. Hadaway and published by . This book was released on 1951 with total page 31 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 Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds by : Lawrence D. Guy
Download or read book Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds written by Lawrence D. Guy and published by . This book was released on 1954 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been made of two unswept, partial-span, flap-type controls (differing only in hinge-line location) mounted on a 60 degree delta wing. One control was unbalanced and the other has a 100-percent overhang balance. Control hinge moments as well as aerodynamic characteristics of the complete wing-body combination were obtained for control deflections from 0 to 40 degrees over an angle-of-attack range of plus or minus 12 degrees at Mach numbers from 0.75 to 1.96. Reynolds numbers varied between 2,200,000 and 2,200,000. Expressions derived from linear theory for the hinge-moment coefficient due to angle of attack for unswept partial-span controls (which extend neither to the wing tip nor to the wing center line) on triangular wings having subsonic leading edges are given in an appendix.
Book Synopsis Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Degrees Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons by : Harold S. Johnson
Download or read book Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Degrees Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons written by Harold S. Johnson and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Low Speed of the Lateral Control Characteristics of Ailerons Having Three Spans and Three Trailing-edge Angles on a Semispan Wing Model by : Leslie E. Schneiter
Download or read book Wind-tunnel Investigation at Low Speed of the Lateral Control Characteristics of Ailerons Having Three Spans and Three Trailing-edge Angles on a Semispan Wing Model written by Leslie E. Schneiter and published by . This book was released on 1948 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presents results of a wind-tunnel investigation of the low-speed lateral control characteristics of an essentiallty unswept wing (leading-edge sweptback 6.3 degrees) equipped with sealed 20-percent-chord plain ailerons having spans of 0.954, 0.583, and 0.294 percent of a full-span aileron, each with trailing-edge angles of 6, 14, and 25 degrees. Experiments were also performed with the ailerons unsealed, used as lift flaps having spans of 0.954 and 0.660 percent of a full-span flap. The aileron hinge-moment s and internal-seal pressures were determined for each of the nine aileron configurations in addition to the usual lift and lateral-control coefficients.
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 Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Degree Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons by : Harold S. Johnson
Download or read book Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Degree Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons written by Harold S. Johnson and published by . This book was released on 1951 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation at low speed was made to determine the lateral control characteristics of a 45 degree sweptback untapered semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain unsealed ailerons. Variations of the lateral-control data with aileron span and spanwise location were determined through a large aileron-deflection range for various angles of attack up to about the angle of maximum lift.
Book Synopsis Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds by : Robert F. Thompson
Download or read book Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds written by Robert F. Thompson and published by . This book was released on 1950 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley high-speed 7- by 10-foot tunnel of 42.7 degrees sweptback wing model to determine the effects of aileron trailing-edge thickness on aileron hinge moments and one-degree-of-freedom aileron flutter. The wing had an aspect ratio of 4.0, a taper ratio of 0.5, and was tested over a Mach number range of 0.60 to 1.175. The half-span, 20-percent-chord ailerons were flat sided and located outboard.
Book Synopsis Investigation of the Hinge-Moment Fluctuations of a 0.20-Chord Plain Ailerons on a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed-Tunnel by :
Download or read book Investigation of the Hinge-Moment Fluctuations of a 0.20-Chord Plain Ailerons on a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed-Tunnel written by and published by . This book was released on 1947 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: Photographic records of hinge moment fluctuations were made by means of an oscillograph connected to an electrical strain gage. At super critical Mach numbers, frequencies of the order of magnitude of 50 to 100 cycles per second were observed for the hinge-moment fluctuations of the aileron of the model. For a 104.5 foot span airplane, full scale hinge-moment-fluctuation frequencies are indicated to be of the same order of magnitude as the wing natural frequencies.
Book Synopsis Effect of a Deflectable Wing-tip Control on the Low-speed Lateral and Longitudinal Characteristics of a Large-scale Wing with the Leading Edge Swept Back 47.5 Degrees by : Roy H. Lange
Download or read book Effect of a Deflectable Wing-tip Control on the Low-speed Lateral and Longitudinal Characteristics of a Large-scale Wing with the Leading Edge Swept Back 47.5 Degrees written by Roy H. Lange and published by . This book was released on 1951 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented of an investigation in the Langley full-scale tunnel of the effect of a 20-percent-semispan deflectable wing-tip control on the low-speed lateral and longitudinal characteristics of a wing with the leading edge swept back 47.5 degrees, an aspect ratio of 3.5, and circular-arc-airfoil sections. Limited tests were also made of a conventional a aileron simulated by an outboard 50-percent-semispan, 20-percent-chord trailing-edge plain flap (for positive deflections only). The basic wing configuration, the wing with drooped-nose flaps deflected 40 degrees, and the wing with drooped-nose and semispan plain flaps deflected 40 degrees were tested in the course of the investigation. All the data are presented for a Reynolds number of 4,300,000 and a Mach number of 0.07.
Book Synopsis Low-speed Investigation of the Effect of Several Flap and Spoiler Ailerons on the Lateral Characteristics of a 47.5 Degrees Sweptback-wing - Fuselage Combination at a Reynolds Number of 4.4 X (10)6 by : Jerome Pasamanick
Download or read book Low-speed Investigation of the Effect of Several Flap and Spoiler Ailerons on the Lateral Characteristics of a 47.5 Degrees Sweptback-wing - Fuselage Combination at a Reynolds Number of 4.4 X (10)6 written by Jerome Pasamanick and published by . This book was released on 1950 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Various Aerodynamic Balances on the Low-speed Lateral-control and Hinge-moment Characteristics of a 0.20 Chord Partial-span Outboard Aileron on a Wing with a Leading Edge Swept Back 51.3 Degrees by : Alexander D. Hammond
Download or read book The Effect of Various Aerodynamic Balances on the Low-speed Lateral-control and Hinge-moment Characteristics of a 0.20 Chord Partial-span Outboard Aileron on a Wing with a Leading Edge Swept Back 51.3 Degrees written by Alexander D. Hammond and published by . This book was released on 1952 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Investigation of Low-speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing with Leading Edge Swept Back 42 Degrees with and Without High-lift Devices by : Thomas V. Bollech
Download or read book Investigation of Low-speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing with Leading Edge Swept Back 42 Degrees with and Without High-lift Devices written by Thomas V. Bollech and published by . This book was released on 1949 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Lateral-control Investigation of a Flap-type Spoiler Aileron with and Without a Deflector and Slot on a 6-percent-thick, Tapered, 45 Degree Sweptback Wing of Aspect Ratio 4 by : James M. Watson
Download or read book Low-speed Lateral-control Investigation of a Flap-type Spoiler Aileron with and Without a Deflector and Slot on a 6-percent-thick, Tapered, 45 Degree Sweptback Wing of Aspect Ratio 4 written by James M. Watson and published by . This book was released on 1952 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley 300 MPH 7- by 10-foot tunnel to determine the lateral control characteristics of a deflector and slot arrangement in conjunction with a flap-type spoiler aileron. The wing had a sweepback of 45 degrees at the quarter-chord line, an aspect ratio of 4, a taper ratio of 0.6, and an NACA 65A006 airfoil section parallel to the free air stream.
