Download or read book Low speed Characteristics in Pitch of a 340 Sweptforward Wing with Circular arc Airfoil Sections written by D. William Conner and published by . This book was released on 1947 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Characteristics in Pitch of a 34 Sweptforward Wing with Circular arc Airfoil Sections written by D. William Conner and published by . This book was released on 1947 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Characteristics in Pitch of a 34 Degrees Sweptforward Wing with Circular arc Airfoil Sections written by D. William Conner and published by . This book was released on 1948 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low Speed Characteristics in Pitch of a 42 Degree Swept Back Wing with Aspect Ratio 3 9 and Circular Arc Airfoil Sections written by and published by . This book was released on 1947 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Characteristics in Pitch of a 42 Degrees Sweptback Wing with Aspect Ratio 3 9 and Circular arc Airfoil Sections written by Robert H. Neely and published by . This book was released on 1947 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Validation of USAF Stability and Control Datcom Methodologies for Straight tapered Sweptforward Wings written by Daniel G. Sharpes and published by . This book was released on 1985 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt: A detailed review of USAF Stability and Control Datcom methodologies was conducted to determine their validity for application to straight tapered, sweptforward wing configurations. To the extent possible the format found in the Datcom is repeated in this report. Several methods were modified to enable more accurate coefficient prediction (e.g., Wing Zero-Lift Angle of Attack, Downwash and Yawing Moment due to Yaw Rate) irrespective of sweep sign. At supersonic speeds, the reversibility theorem enabled most methodologies to be used without any modifications to account for sweptforward leading-edge designs. For the methodologies validated, sweptforward-wing estimation results were generally as accurate as the sweptback-wing results presented in the Datcom. Unfortunately, lack of test data prevented validation of several empirical methodologies (e.g., Subsonic High Angle-of-Attack Pitching Moment and Transonic Pitching Moment). No estimation methodologies are proposed in these cases.

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.

Download or read book Summary and Analysis of Horizontal tail Contribution to Longitudinal Stability of Swept wing Airplanes at Low Speeds written by Robert H. Neely and published by . This book was released on 1959 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Air-flow characteristics behind wings and wing-body combinations are described and are related to the downwash at specific tail locations for unseparated and separated flow conditions. The effects of various parameters and control devices on the air-flow characteristics and tail contribution are analyzed and demonstrated. An attempt has been made to summarize certain data in a form useful for design. The experimental data herein were obtained mostly at Reynolds numbers greater than 4 x 105 and at Mach numbers less than 0.25.

Download or read book Low speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular arc Airfoil Sections at Reynolds of Approximately 6 0 X 10 6 written by Stanley H. Spooner and published by . This book was released on 1949 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low Speed Aerodynamic Characteristics of a Forward Swept Wing Aircraft written by I.R. Tuckwell and published by . This book was released on 1984 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Exploratory Investigation of the Low speed Aerodynamic Characteristics of Variable wing Sweep Airplane Configurations written by and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Pressure Distributions Over the Drooped nose Flap of a 42 Degree Sweptback Wing with Circular arc Airfoil Sections at a Reynolds Number of 5 3 X 10 6 written by Stanley H. Spooner and published by . This book was released on 1948 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Aerodynamic Characteristics of a Generic Forward swept wing Aircraft written by J. C. Ross and published by . This book was released on 1982 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Aerodynamic Characteristics of a Series of Swept Wings Having NACA 65A006 Airfoil Sections written by Jones F. Cahill and published by . This book was released on 1950 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Longitudinal Characteristics of a Circular arc 52 Degrees Sweptback Wing of Aspect Ratio 2 84 with and Without Leading edge and Trailing edge Flaps at Reynolds Number from 1 6 X 10 6 to 9 7 X 10 6 written by Gerald V. Foster and published by . This book was released on 1950 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Lateral Control Characteristics of an Unswept Wing with Hexagonal Airfoil Sections and Aspect Ratio 4 0 at a Reynolds Number of 6 2 X 10 6 written by William M. Hadaway and published by . This book was released on 1953 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: