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Wind Tunnel Investigation At Low Speed Of The Lateral Control Characteristics Of An Unswept Untapered Semispan Wing Of Aspect Ratio 313 Equipped With Various 25 Percent Chord Plain Ailerons
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Book Synopsis Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 [degress] 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 [degress] 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 1950 with total page 30 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 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:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1952 with total page 810 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Low Speed of a 45° Sweptback Untapered Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Flaps by : Harold S. Johnson
Download or read book Wind-tunnel Investigation at Low Speed of a 45° Sweptback Untapered Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Flaps written by Harold S. Johnson and published by . This book was released on 1950 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of the Effect of Control Span and Large Wing-tip Nacelles on Effectiveness of Spoiler-slot- Deflector Controls on an Unswept-wing Fighter-type Airplane by :
Download or read book Transonic Wind-tunnel Investigation of the Effect of Control Span and Large Wing-tip Nacelles on Effectiveness of Spoiler-slot- Deflector Controls on an Unswept-wing Fighter-type Airplane written by and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Low-speed Longitudinal and Lateral Control Characteristics of a Triangular-wing Model of Aspect Ratio 2.31 Having Constant-chord Control Surfaces by : Walter D. Wolhart
Download or read book Wind-tunnel Investigation of the Low-speed Longitudinal and Lateral Control Characteristics of a Triangular-wing Model of Aspect Ratio 2.31 Having Constant-chord Control Surfaces written by Walter D. Wolhart and published by . This book was released on 1950 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of an Unswept Wing in Combination with a Systematic Series of Four Bodies by : Bruce B. Estabrooks
Download or read book Transonic Wind-tunnel Investigation of an Unswept Wing in Combination with a Systematic Series of Four Bodies written by Bruce B. Estabrooks and published by . This book was released on 1953 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Deg Swept Leading Edge by :
Download or read book Low-speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Deg Swept Leading Edge written by and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg by :
Download or read book Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg written by and published by . This book was released on 1995 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Wind-tunnel Investigation of Aerodynamic-loading Characteristics of a 2-percent-thick Trapezoidal Wing in Combination with Basic and Indented Bodies by : Thomas C. Kelly
Download or read book Transonic Wind-tunnel Investigation of Aerodynamic-loading Characteristics of a 2-percent-thick Trapezoidal Wing in Combination with Basic and Indented Bodies written by Thomas C. Kelly and published by . This book was released on 1957 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.
Book Synopsis Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics by : Isidore G. Recant
Download or read book Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics written by Isidore G. Recant and published by . This book was released on 1942 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were tested in the NACA 7- by 10-foot wind tunnel to determine the effect of wing-fuselage interference on the lateral-stability of wing-fuselage interference on the lateral-stability characteristics. The model configurations represented a high-wing, a mid-wing, and a low-wing monoplane. For each configuration, tests were made with a partial-span split flap neutral and deflected 60 degrees and with and without a vertical tail. Tests of the fuselage alone and of the fuselage with the vertical tail were also made.
Book Synopsis Low-speed Wind-tunnel Tests on an Unswept Wing-fuselage Model of Aspect Ratio 9.8, with Tangential Blowing Over Trailing-edge Flaps and Ailerons, Including the Effect of Slipstream by : J. A. Lawford
Download or read book Low-speed Wind-tunnel Tests on an Unswept Wing-fuselage Model of Aspect Ratio 9.8, with Tangential Blowing Over Trailing-edge Flaps and Ailerons, Including the Effect of Slipstream written by J. A. Lawford and published by . This book was released on 1970 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation at High Subsonic Speeds of the Lateral Control Characteristics of Various Plain Spoiler Configurations on a 3-percent-thick 60 Degree Delta Wing by : Harleth G. Wiley
Download or read book A Wind-tunnel Investigation at High Subsonic Speeds of the Lateral Control Characteristics of Various Plain Spoiler Configurations on a 3-percent-thick 60 Degree Delta Wing written by Harleth G. Wiley and published by . This book was released on 1954 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12 Foot Pressure Wind Tunnel by : Ben H. Jr Johnson
Download or read book Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12 Foot Pressure Wind Tunnel written by Ben H. Jr Johnson and published by . This book was released on 1948 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences by : James A. Weilberg
Download or read book Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences written by James A. Weilberg and published by . This book was released on 1952 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel and Analytical Investigation of Over-the-wing Propulsion/air Frame Interferences for a Short-haul Aircraft at Mach Numbers from 0.6 to 0.78 by : O. D. Wells
Download or read book Wind Tunnel and Analytical Investigation of Over-the-wing Propulsion/air Frame Interferences for a Short-haul Aircraft at Mach Numbers from 0.6 to 0.78 written by O. D. Wells and published by . This book was released on 1977 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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