Flight Determination Of The Drag And Longitudinal Stability And Control Characteristics Of A Rocket Powered Model Of A 60 Degrees Delta Wing Airplane From Mach Numbers Of 0 75 To 1 70
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Government Reports Index
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Author :
language : en
Publisher:
Release Date : 1973
Government Reports 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 1973 with Government publications categories.
Flight Determination Of The Drag And Longitudinal Stability And Control Characteristics Of A Rocket Powered Model Of A 60 Degrees Delta Wing Airplane From Mach Numbers Of 0 75 To 1 70
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Author : Grady L. Mitcham
language : en
Publisher:
Release Date : 1951
Flight Determination Of The Drag And Longitudinal Stability And Control Characteristics Of A Rocket Powered Model Of A 60 Degrees Delta Wing Airplane From Mach Numbers Of 0 75 To 1 70 written by Grady L. Mitcham and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 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.
Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1952
Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Have A 60 Delta Wing And A High Unwept Horizontal Tail
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Author : Robert F. Peck
language : en
Publisher:
Release Date : 1953
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Have A 60 Delta Wing And A High Unwept Horizontal Tail written by Robert F. Peck and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Delta wing 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.
Importants Manuscrits Et Documents Relatifs La Bastille Et Au Faubourg Saint Antoine
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Author :
language : en
Publisher:
Release Date : 1985
Importants Manuscrits Et Documents Relatifs La Bastille Et Au Faubourg Saint Antoine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with categories.
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Having A 60 Degree Delta Wing And A High Unswept Horizontal Tail
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Author : Robert F. Peck
language : en
Publisher:
Release Date : 1953
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Having A 60 Degree Delta Wing And A High Unswept Horizontal Tail written by Robert F. Peck and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 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.
Results Of A Flight Investigation To Determine The Zero Lift Drag Characteristics Of A 60 Degree Delta Wing With Naca 65 006 Airfoil Section And Various Double Wedge Sections At Mach Numbers From 0 7 To 1 6
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Author : Clement J. Welsh
language : en
Publisher:
Release Date : 1956
Results Of A Flight Investigation To Determine The Zero Lift Drag Characteristics Of A 60 Degree Delta Wing With Naca 65 006 Airfoil Section And Various Double Wedge Sections At Mach Numbers From 0 7 To 1 6 written by Clement J. Welsh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerofoils 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.