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 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 Aerodynamic Characteristics at a Mach Number of 2 01 of a Variable sweep Airplane Configuration with Body mounted Podded Engines and Having an Equivalentbody Fineness Ratio of 9 8 written by and published by . This book was released on 1962 with total page 22 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 Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable sweep Wing Having an M Planform written by William P. Henderson and published by . This book was released on 1964 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Aerodynamic Characteristics of a Variable sweep Airplane Configuration Having a 12 percent thick Wing and an Inboard Pivot Location written by Ralph P. Bielat and published by . This book was released on 1960 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1961-10 with total page 1540 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability and Control Characteristics at Transonic Speeds of Two Variable sweep Airplane Configurations Differing in Wing pivot Locations written by Ralph P. Bielat and published by . This book was released on 1961 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability Characteristics at Mach 2 20 of a Variable sweep Configuration Having Pylon mounted Nacelles with Conical Inlets written by and published by . This book was released on 1965 with total page 76 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 1206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2 20 of a V STOL Airplane Configuration with a Variable sweep Wing and with a Skewed Wing Design written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2 20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary Variable sweep Wing Panels written by and published by . This book was released on 1963 with total page 44 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 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability and Control Characteristics at a Mach Number of 2 01 of a Variable sweep Airplane Configuration Capable of Low level Supersonic Attack Outer Wing Swept 75 Deg written by and published by . This book was released on 1960 with total page 24 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 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:
