Free Flight Investigation At Mach Numbers From 0 8 To 1 5 Of The Effect Of A Fuselage Indentation On The Zero Lift Drag Of A 52 5 Degree Sweptback Wing Body Configuration With Symmetrically Mounted Stores On The Fuselage
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Free Flight Investigation At Mach Numbers From 0 8 To 1 5 Of The Effect Of A Fuselage Indentation On The Zero Lift Drag Of A 52 5 Degree Sweptback Wing Body Configuration With Symmetrically Mounted Stores On The Fuselage
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Author : Sherwood Hoffman
language : en
Publisher:
Release Date : 1958
Free Flight Investigation At Mach Numbers From 0 8 To 1 5 Of The Effect Of A Fuselage Indentation On The Zero Lift Drag Of A 52 5 Degree Sweptback Wing Body Configuration With Symmetrically Mounted Stores On The Fuselage written by Sherwood Hoffman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with categories.
Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile
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Author : Eugene D. Schult
language : en
Publisher:
Release Date : 1960
Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile 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 1960 with Mach number categories.
Free Flight Tests At Mach Numbers From 0 8 To 1 4 To Determine The Effect On Zero Lift Drag Of Increasing The Leading Edge Bluntness Of A 45 Degree Sweptback Wing Having An Naca 65a009 Airfoil
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Author : William B. Pepper
language : en
Publisher:
Release Date : 1952
Free Flight Tests At Mach Numbers From 0 8 To 1 4 To Determine The Effect On Zero Lift Drag Of Increasing The Leading Edge Bluntness Of A 45 Degree Sweptback Wing Having An Naca 65a009 Airfoil written by William B. Pepper 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.
A Flight Investigation Of The Transonic Area Rule For A 52 5 Sweptback Wind Body Configuration At Mach Numbers Between 0 8 And 1 6
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Author : Sherwood Hoffman
language : en
Publisher:
Release Date : 1954
A Flight Investigation Of The Transonic Area Rule For A 52 5 Sweptback Wind Body Configuration At Mach Numbers Between 0 8 And 1 6 written by Sherwood Hoffman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics, Transonic 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.
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 : 1960
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 1960 with Aerodynamics categories.
Lift And Drag Of The Bell X 5 Research Airplane In The 45 Degree Sweptback Configuration At Transonic Speeds
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Author : Jack Nugent
language : en
Publisher:
Release Date : 1956
Lift And Drag Of The Bell X 5 Research Airplane In The 45 Degree Sweptback Configuration At Transonic Speeds written by Jack Nugent and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics, Transonic categories.
A flight investigation was made of the Bell X-5 variable sweep research airplanes in the 45 degree wing sweptback configuration over a Mach number range from 0.61 to 1.01. Lift and drag values are presented and a comparison is made with data previously obtained with a wing sweepback of 59 degrees.
Flight Investigation At Mach Numbers From 0 8 To 1 4 To Determine The Zero Lift Drag Of Wings With M And W Plan Forms
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Author : Ellis Katz
language : en
Publisher:
Release Date : 1950
Flight Investigation At Mach Numbers From 0 8 To 1 4 To Determine The Zero Lift Drag Of Wings With M And W Plan Forms written by Ellis Katz 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 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 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.