Comparison Of Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 9 To 1 7 Of Two Wing Body Combinations Having Similar 60 Degree Triangular Wings With Naca 65a003 Sections
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Comparison Of Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 9 To 1 7 Of Two Wing Body Combinations Having Similar 60 Degree Triangular Wings With Naca 65a003 Sections
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Author : Eugene D. Schult
language : en
Publisher:
Release Date : 1950
Comparison Of Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 9 To 1 7 Of Two Wing Body Combinations Having Similar 60 Degree Triangular Wings With Naca 65a003 Sections written by Eugene D. Schult and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with categories.
Comparison Of Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 9 To 1 7 Of Two Wing Body Combinations Having Similar 60 Degrees Triangular Wings With Naca 65a003 Sections
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Author : Eugene D. Schult
language : en
Publisher:
Release Date : 1951
Comparison Of Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 9 To 1 7 Of Two Wing Body Combinations Having Similar 60 Degrees Triangular Wings With Naca 65a003 Sections written by Eugene D. Schult 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.
Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 86 To 1 5 Of A Wing Body Combination Having A 60 Degree Triangular Wing With Naca 65a003 Sections
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Author : Robert L. Nelson
language : en
Publisher:
Release Date : 1950
Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 86 To 1 5 Of A Wing Body Combination Having A 60 Degree Triangular Wing With Naca 65a003 Sections written by Robert L. Nelson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with categories.
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.
Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 86 To 1 5 Of A Wing Body Combination Having A 60 Degrees Triangular Wing With Naca 65a003 Sections
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Author : Robert L. Nelson
language : en
Publisher:
Release Date : 1951
Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 86 To 1 5 Of A Wing Body Combination Having A 60 Degrees Triangular Wing With Naca 65a003 Sections written by Robert L. Nelson 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.
Free Flight Measurements Of The Zero Lift Drag Of Several Wings At Mach Numbers From 1 4 To 3 8
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Author : H. Herbert Jackson
language : en
Publisher:
Release Date : 1960
Free Flight Measurements Of The Zero Lift Drag Of Several Wings At Mach Numbers From 1 4 To 3 8 written by H. Herbert Jackson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Mach number categories.
Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 8 To 1 6 Of A Wing Body Combination Having An Unswept 4 5 Percent Thick Wing With Modified Hexagonal Sections
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Author : Eugene D. Schult
language : en
Publisher:
Release Date : 1951
Large Scale Flight Measurements Of Zero Lift Drag At Mach Numbers From 0 8 To 1 6 Of A Wing Body Combination Having An Unswept 4 5 Percent Thick Wing With Modified Hexagonal Sections written by Eugene D. Schult 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.
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0
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Author : Robert S. Osborne
language : en
Publisher:
Release Date : 1953
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0 written by Robert S. Osborne 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.
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.
The Zero Lift Drag Of A 60 Degree Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7
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Author : Robert O. Piland
language : en
Publisher:
Release Date : 1954
The Zero Lift Drag Of A 60 Degree Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7 written by Robert O. Piland and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
The zero-lift drag of a 60 degree delta-wing-body combination (designated AGARD Model 2) has been determined by free-flight tests of two models between Mach numbers of 0.8 and 1.7. These Mach numbers correspond to Reynolds numbers, based on body length, of 4,000,000 and 12,000,000, respectively. An estimate of the drag of the configuration was made by summing the estimates of the drag of the various components. The agreement between measured and estimated drag is good.