Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 01 Of A Series Of Cranked Wings Ranging In Aspect Ratio From 4 00 To 1 74 In Combination With A Body
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Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 01 Of A Series Of Cranked Wings Ranging In Aspect Ratio From 4 00 To 1 74 In Combination With A Body
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Author : John R. Sevier
language : en
Publisher:
Release Date : 1960
Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 01 Of A Series Of Cranked Wings Ranging In Aspect Ratio From 4 00 To 1 74 In Combination With A Body written by John R. Sevier 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, Supersonic categories.
Aerodynamic Characteristics Of Several Cranked Leading Edge Wing Body Combinations At Mach Numbers From 0 4 To 2 94
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Author : Edward J. Hopkins
language : en
Publisher:
Release Date : 1967
Aerodynamic Characteristics Of Several Cranked Leading Edge Wing Body Combinations At Mach Numbers From 0 4 To 2 94 written by Edward J. Hopkins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Airplanes categories.
Longitudinal Aerodynamic Characteristics At Mach Number 2 02 Of A Series Of Wing Body Configurations Employing A Cambered And Twisted Arrow Wing
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Author : Harry W. Carlson
language : en
Publisher:
Release Date : 1963
Longitudinal Aerodynamic Characteristics At Mach Number 2 02 Of A Series Of Wing Body Configurations Employing A Cambered And Twisted Arrow Wing written by Harry W. Carlson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with categories.
Aerodynamic Characteristics In Pitch Of Several M Wing Body Combinations At Mach Numbers Of 2 40 2 60 And 2 86
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Author : Odell A. Morris
language : en
Publisher:
Release Date : 1965
Aerodynamic Characteristics In Pitch Of Several M Wing Body Combinations At Mach Numbers Of 2 40 2 60 And 2 86 written by Odell A. Morris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamics 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.
Transonic Aerodynamic Characteristics Of A Wing Body Combination Having A 52 2 Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of 2
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Author : William B. Igoe
language : en
Publisher:
Release Date : 1961
Transonic Aerodynamic Characteristics Of A Wing Body Combination Having A 52 2 Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of 2 written by William B. Igoe and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
The Aerodynamic Characteristics Of Several Thick Delta Wings At Mach Numbers To 6 And Angles Of Attack 50
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Author : John B. McDevitt
language : en
Publisher:
Release Date : 1960
The Aerodynamic Characteristics Of Several Thick Delta Wings At Mach Numbers To 6 And Angles Of Attack 50 written by John B. McDevitt 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.
Off Design Aerodynamic Characteristics At Mach Numbers 1 61 And 2 20 Of A Series Of Highly Swept Arrow Wings Designed For Mach Number 2 0 Employing Various Degrees Of Twist And Camber
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Author : Wilbur D. Middleton
language : en
Publisher:
Release Date : 1963
Off Design Aerodynamic Characteristics At Mach Numbers 1 61 And 2 20 Of A Series Of Highly Swept Arrow Wings Designed For Mach Number 2 0 Employing Various Degrees Of Twist And Camber written by Wilbur D. Middleton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics, Supersonic categories.
Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4
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Author : Clarence L. Gillis
language : en
Publisher:
Release Date : 1959
Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4 written by Clarence L. Gillis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Mach number categories.
Aerodynamic Characteristics Of Four Wings Of Sweepback Angles 0 Degrees 35 Degrees 45 Degrees And 60 Degrees Naca 65a006 Airfoil Section Aspect Ratio 4 And Taper Ratio 0 6 In Combination With A Fuselage At High Subsonic Mach Numbers And At A Mach Number Of 1 2
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Author : Arvo A. Luoma
language : en
Publisher:
Release Date : 1951
Aerodynamic Characteristics Of Four Wings Of Sweepback Angles 0 Degrees 35 Degrees 45 Degrees And 60 Degrees Naca 65a006 Airfoil Section Aspect Ratio 4 And Taper Ratio 0 6 In Combination With A Fuselage At High Subsonic Mach Numbers And At A Mach Number Of 1 2 written by Arvo A. Luoma 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.