Download or read book Wind tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing fuselage Combination with Quarter chord Line Swept Back 32 6 Degrees and NACA 65A006 Airfoil Section written by Harold S. Johnson and published by . This book was released on 1953 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book WIND TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER SLOT DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER CHORD LINE SWEPT BACK 32 6 written by and published by . This book was released on 1953 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation at High Subsonic Speeds of Spoilers of Large Projection on an NACA 65A006 Wing with Quarter chord Line Swept Back 32 6 Degrees written by Raymond D. Vogler and published by . This book was released on 1952 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation at High Subsonic Speeds of a Spoiler slot deflector Combination on an NACA 65A006 Wing with Quarter chord Line Swept Back 32 6 Degrees written by Raymond D. Vogler and published by . This book was released on 1953 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation to Determine the Horizontal and Vertical tail Contributions to the Static Lateral Stability Characteristics of a Complete model Swept wing Configuration at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1956 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral stability of a complete-model swept-wing configuration at high subsonic speeds. The results indicate that, in a general, Mach number effects within the range studied and wing effects on the tail contribution were small and the overall trends of the data of the present investigation agreed with those which have been established at low speeds.

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:

Download or read book Wind tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing written by Thomas J. Jr King and published by . This book was released on 1956 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing fuselage Combination Having a Triangular Wing of Aspect Ratio 2 31 and an NACA 65A003 Airfoil written by James W. Wiggins and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation at High Subsonic Speeds of the Effects of Wing mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined with a Fuselage written by H. Norman Silvers and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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.

Download or read book Loads on Wings Due to Spoilers at Subsonic and Transonic Speeds written by Alexander D. Hammond and published by . This book was released on 1955 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Investigation of the Lateral control Characteristics of a Flap type Spoiler and a Spoiler slot Deflector on a 30 Degree Sweptback Wing fuselage Model Having an Aspect Ratio of 3 a Taper Ratio of 0 5 and NACA 65A004 Airfoil Section written by Alexander D. Hammond and published by . This book was released on 1956 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been made at low speed in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of deflector projection on the control effectiveness of spoiler-slot-deflectors on a 30 degree sweptback wing-fuselage model equipped with either a 15-percent-chord spoiler or a spoiler-slot-deflector that extended from the 20- to the 99-percent-semispan station of the right ring. The wing had an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section. The tests were made at angles of attack from -4 to 24 degrees at Mach number of 0.26 for control projections from 0 to 12 percent chord. The deflector of the spoiler-slot-deflector configuration was tested at projections from zero to a projection equal to the spoiler projection at each spoiler projection.

Download or read book A Transonic wing Investigation in the Langley 8 foot High speed Tunnel at High Subsonic Mach Numbers and at Mach Numbers of 1 2 written by Raymond B. Wood and published by . This book was released on 1951 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation of the Static Lateral Stability Characteristics of Wing fuselage Combinations at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1953 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation to Determine the Horizontal and Vertical tail Contributions to the Static Lateral Stability Characteristics of a Complete model Swept wing Configuration at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1953 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind Tunnel Investigation of Control Surface Characteristics written by H. Page Hoggard and published by . This book was released on 1943 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Force-test measurements in two-dimensional flow have been made in the NACA 4- by 6-foot vertical tunnel to determine the aerodynamic effects of changing the alignment of the cover plates on a sealed internally balanced flap. An NACA 0015 airfoil was utilized for the tests. The chord of the straight-contour flap was 30 percent of the airfoil chord and the balance with 50 percent of the flap chord.

Download or read book A Transonic wing Investigation in the Langley 8 foot High speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1 2 written by Maurice S. Cahn and published by . This book was released on 1951 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: