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 the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing fuselage Combination Winter Quarter chord Line Swept Back 32 6 and NACA 65A006 Airfoil Section written by Harold S. Johnson and published by . This book was released on 1953 with total page 20 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 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 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 at High Subsonic Speeds of the Lateral control Characteristics of an Aileron and a Stepped Spoiler on a Wing with Leading Edge Swept Back 51 3 Degrees written by Leslie E. Schneiter and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been made through a speed range from a Mach number of approximately 0.90 to determine the lateral-control characteristics of a 2-percent-chord by 39-percent-semispan aileron and a 60-percent-semispan stepped spoiler on a semispan-wing model with aspect ratio of 3.06 having 51.3 degree sweepback of the wing leading edge. In addition, the aerodynamic characteristics of the plain wing were determined through the speed range.

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 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 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 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 1957 with total page 25 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 Wind tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13 Degrees and at High Subsonic Mach Numbers Including a Semiempirical Method of Estimating the Rolling Derivatives written by James W. Wiggins and published by . This book was released on 1958 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was performed in the Langley high-speed 7- by 10-foot tunnel in order to determine the rolling derivatives for swept-wing-body configurations at angles of attack from 0 degrees to 13 degrees and at high subsonic Mach numbers. The wings had sweep angles of 3.6 degrees, 32.6 degrees, 45 degrees, and 60 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 stream. The results indicate a reduction in the damping-in-roll derivative at the higher test angles of attack. Of the wings tested, instability of the damping-in-roll derivative was experienced over the largest ranges of angle of attack and Mach number for the 32.6 sweptback wing.

Download or read book Wind tunnel Studies at Subsonic and Transonic Speeds of a Multiple mission Variable wing Sweep Airplane Configuration written by William J. Alford and published by . This book was released on 1959 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing fuselage Combinations at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1952 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: