Download or read book The Effects of Horizontal tail Position on the Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Variable sweep Aircraft Having an Inboard Pivot written by Alexander D. Hammond and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Wing Sweep and Horizontal tail Position on the Aerodynamic Characteristics at a Mach Number of 2 2 of a Variable sweep Airplane Configuration Having an Inboard Wing Pivot written by M. Leroy Spearman and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Proceedings of NASA Conference on Supersonic Transport Feasibility Studies and Supporting Research September 17 19 1963 Langley Research Center Langley Station Hampton Va written by and published by . This book was released on 1963 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Summary of Research on Variable sweep Fighter Airplanes written by and published by . This book was released on 1965 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Aerodynamic Characteristics of a Double pivot Variable wing sweep Airplane Configuration Having Conventional and Outboard Horizontal Tail Surfaces written by William P. Henderson and published by . This book was released on 1963 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Horizontal tail Height on Aerodynamic Characteristics of a Transport Model with a Variable sweep Warped Wing written by and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Longitudinal Aerodynamic Characteristics of a Variable sweep Fighter Model Having Body mounted Nacelles written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Wind tunnel Investigation of the Aerodynamic Characteristics of a Hypersonic Airplane Model with Variable Wing Geometry written by William J. Jr Alford and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable Sweep Wing Having an M Planform written by and published by . This book was released on 1964 with total page 46 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 1967 with total page 1582 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Proceedings of NASA Conference on Supersonic transport Feasibility Studies and Supporting Research written by and published by . This book was released on 1963 with total page 526 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of Non straight taper Wings written by David B. Benepe and published by . This book was released on 1966 with total page 322 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.
Download or read book Effects of Wing pivot Location and Forewing Configuration on the Low speed Aerodynamic Characteristics of a Variable sweep Airplane Model written by Jarrett K. Huffman and published by . This book was released on 1972 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made to determine the effects of the location of the wing pivot and geometry of the forewing on the static longitudinal aerodynamic characteristics at subsonic speeds of a model representing a variable-sweep supersonic fighter airplane. Results indicate that as the wing-pivot location moves aft and outboard, the change in static margin due to wing sweep is reduced. Increasing the forewing area resulted in a forward shift of the aerodynamic center as well as a slight reduction in the aerodynamic-center variation due to wing sweep.--P. [i].
Download or read book Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Swept wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail written by M. Leroy Spearman and published by . This book was released on 1957 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
Download or read book USAF Stability and Control Datcom written by Douglas Aircraft Company and published by . This book was released on 1975 with total page 588 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Horizontal tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip written by Donald R. Riley and published by . This book was released on 1953 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley stability tunnel on a vertical-tail model with a stub fuselage in combination with various horizontal tails to determine the effect of horizontal-tail span and vertical location of the horizontal tail relative to the vertical tail on the aerodynamic characteristics of an unswept tail assembly in sideslip.
