Download or read book Low speed Investigation of the Effects of Wing Flap Deflection and Horizontal tail Configuration on the Longitudinal Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips written by William C. Jr Hayes and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Effects of High lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model with Outboard Tails written by William C. Sleeman and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing edge Flap Controls in Combination written by Bernard Spencer and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1961 with total page 1196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Effects of High lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model with Outboard Tails written by and published by . This book was released on 1963 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Investigation of the Effects of Horizontal tail Area and Wing Sweep on the Static Longitudinal Stability and Control Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips written by William C. Jr Hayes and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of a Transport Airplane Configuration Having Tail Surfaces Located Outboard of the Wing Tips at Mach Numbers of 2 30 2 96 3 95 and 4 63 written by and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Exploratory Study of a Parawing as a High lift Device for Aircraft written by Rodger L. Naeseth and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1979 with total page 1074 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1967 with total page 2300 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low Speed Aerodynamic Characteristics of a Modified Arrow wing Supersonic Transport Configuration with High Lift Devices written by and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Investigation of Effects of Wing Leading and Trailing edge Flap Deflections and Canard Incidence on a Fighter Configuration Equipped with a Forward swept Wing written by Thomas G. Gainer and published by . This book was released on 1984 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Horizontal tail Size and Tail Length on Low speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Sweptback Wing and Tail Surfaces written by Jacob H. Lichtenstein and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.
Download or read book A Simplified Method for Estimating Subsonic Lift curve Slope at Low Angles of Attack for Irregular Planform Wings written by Bernard Jr Spencer and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0 25 to 4 63 written by and published by . This book was released on 1983 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
