Stability And Drag Characteristics At Mach Numbers From 0 8 To 1 5 Of A Free Flight Model Having 3 Percent Thick 60 Degree Triangular Wing And Horizontal Tail Surfaces
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Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1987-12
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987-12 with Science categories.
Flying Magazine
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Author :
language : en
Publisher:
Release Date : 2002-08
Flying Magazine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002-08 with categories.
Flying Magazine
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Author :
language : en
Publisher:
Release Date : 2002-08
Flying Magazine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002-08 with categories.
Popular Mechanics
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Author :
language : en
Publisher:
Release Date : 2000-01
Popular Mechanics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000-01 with categories.
Popular Mechanics inspires, instructs and influences readers to help them master the modern world. Whether it’s practical DIY home-improvement tips, gadgets and digital technology, information on the newest cars or the latest breakthroughs in science -- PM is the ultimate guide to our high-tech lifestyle.
Flying Magazine
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Author :
language : en
Publisher:
Release Date : 1966-11
Flying Magazine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966-11 with categories.
Backpacker
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Author :
language : en
Publisher:
Release Date : 2000-03
Backpacker written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000-03 with categories.
Backpacker brings the outdoors straight to the reader's doorstep, inspiring and enabling them to go more places and enjoy nature more often. The authority on active adventure, Backpacker is the world's first GPS-enabled magazine, and the only magazine whose editors personally test the hiking trails, camping gear, and survival tips they publish. Backpacker's Editors' Choice Awards, an industry honor recognizing design, feature and product innovation, has become the gold standard against which all other outdoor-industry awards are measured.
Longitudinal Aerodynamic Characteristics At Mach Numbers From 0 50 To 1 19 Of A Supersonic Transport Model With A Modified M Wing
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Author : Edward J. Ray
language : en
Publisher:
Release Date : 1967
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.
Results Of A Flight Investigation To Determine The Zero Lift Drag Characteristics Of A 60 Deg Delta Wing With Naca 65 006 Airfoil Section And Various Double Wedge Sections At Mach Numbers From 0 7 1 6
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Author :
language : en
Publisher:
Release Date : 1956
Results Of A Flight Investigation To Determine The Zero Lift Drag Characteristics Of A 60 Deg Delta Wing With Naca 65 006 Airfoil Section And Various Double Wedge Sections At Mach Numbers From 0 7 1 6 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with categories.
Results of an exploratory free-flight investigation at zero lift of several rocket-powered drag-research models equipped with 60 deg sweptback delta wings are presented for a Mach number range from about 0.70 to 1.60. The airfoil sections tested included the NACA 65-006 and a series of double-wedge sections with various thicknesses and positions of maximum thickness. The results of the investigation showed that, of the double-wedge sections with 6 percent thickness, the two sections with positions of maximum thickness at 20 and 50 percent of the chord had drag coefficients approximately equal through the transonic and supersonic Mach number range and had similarly occurring drag rises. The section with position of maximum thickness at 80 percent chord had a drag rise occurring at a Mach number M of approximately 0.15 lower than the drag rise of the other two sections. At M = 1.0, this section had drag coefficients more than twice as large as those of the other two sections; however, this difference decreased with increasing supersonic Mach numbers. The wing drag calculated by the linearized theory was in qualitative agreement with the test results in indicating the effects of varying the position of maximum thickness. The double-wedge section of 5 percent thickness with position of maximum thickness at 50 percent chord had fairly constant drag coefficients throughout the supersonic region, which ranged from about 50 to 80 percent of the drag coefficients for the similar section with twice the thickness ratio. The theoretical wing drag for this section was in very good agreement with the experimental value. The NACA 65-006 airfoil section had lower drag coefficients throughout the test region than any of the double-wedge sections of the same thickness ratio, although at the highest Mach numbers covered by these tests, the differences became very small.
Large Scale Flight Measurements Of Zero Lift Drag And Low Lift Drag Of 10 Wing Body Configurations At Mach Numbers From 0 8 To 1 6
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Author : John D. Morrow
language : en
Publisher:
Release Date : 1953
Large Scale Flight Measurements Of Zero Lift Drag And Low Lift Drag Of 10 Wing Body Configurations At Mach Numbers From 0 8 To 1 6 written by John D. Morrow and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.
Effect Of External Stores On The Stability And Control Characteristics Of A Delta Wing Fighter Model At Mach Numbers From 0 60 To 2 01
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Author :
language : en
Publisher:
Release Date : 1983
Effect Of External Stores On The Stability And Control Characteristics Of A Delta Wing Fighter Model At Mach Numbers From 0 60 To 2 01 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.