Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3 00 3 96 and 4 65 of a Low fineness ratio Elliptical Hypersonic Configuration Having 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 Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0 60 to 4 63 for Two Variable sweep Configurations written by and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0 40 to 1 10 of a Blunted Right trangular Pyramidal Lifting Reentry Configuration Employing Variable sweep Wing Panels written by Bernard Spencer and published by . This book was released on 1963 with total page 80 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 Odell A. Morris 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 Aerodynamic Characteristics at Mach Numbers from 0 50 to 2 96 of a Supersonic Transport Model with a Variable sweep High panel aspect ratio Wing written by and published by . This book was released on 1964 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0 50 to 1 19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0 60 to 2 20 of a Variable Sweep Fighter Model with Wing Sweep Angles from 25 Deg to 75 Deg written by and published by . This book was released on 1962 with total page 28 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 Variable wing sweep STOL Configuration written by Gerald V. Foster and published by . This book was released on 1960 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 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 Longitudinal Aerodynamic Characteristics at Mach Numbers from 0 28 to 2 50 of a Multipurpose Tactical Airplane Configuration Having Variable sweep Wings and Externally Mounted Engines written by and published by . This book was released on 1963 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10 03 of Low aspect ratio Wing body Configurations Suitable for Reentry written by and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics at a Mach Number of 2 20 of a Variable sweep Fighter Model with Wing Sweep of 50 Deg 60 Deg and 75 Deg written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics at Mach Numbers of 1 5 1 8 and 2 0 of a Blended Wing body Configuration with and Without Integral Canards written by A. Warner Robins and published by . This book was released on 1979 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 2 36 and 2 86 of a Variable Sweep Airplane Configuration Having Vertical Ramp Inlets written by and published by . This book was released on 1963 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics of Several High drag Bodies at Mach Numbers from 1 50 to 4 63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics of Three Representative Hypersonic Cruise Configurations at Mach Numbers from 0 65 to 10 70 written by and published by . This book was released on 1970 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Performance and Static Stability at Mach Number 3 3 of an Aircraft Configuration Employing Three Triangular Wing Panels and a Body Equal Length written by Carlton S. James and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: An aircraft configuration, previously conceived as a means to achieve favorable aerodynamic stability characteristics., high lift-drag ratio, and low heating rates at high supersonic speeds., was modified in an attempt to increase further the lift-drag ratio without adversely affecting the other desirable characteristics. The original configuration consisted of three identical triangular wing panels symmetrically disposed about an ogive-cylinder body equal in length to the root chord of the panels. This configuration was modified by altering the angular disposition of the wing panels, by reducing the area of the panel forming the vertical fin, and by reshaping the body to produce interference lift. Six-component force and moment tests of the modified configuration at combined angles of attack and sideslip were made at a Mach number of 3.3 and a Reynolds number of 5.46 million. A maximum lift-drag ratio of 6.65 (excluding base drag) was measured at a lift coefficient of 0.100 and an angle of attack of 3.60. The lift-drag ratio remained greater than 3 up to lift coefficient of 0.35. Performance estimates, which predicted a maximum lift-drag ratio for the modified configuration 27 percent greater than that of the original configuration, agreed well with experiment. The modified configuration exhibited favorable static stability characteristics within the test range. Longitudinal and directional centers of pressure were slightly aft of the respective centroids of projected plan-form and side area.
