Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 2 36 And 2 86 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets
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Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1965
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aeronautics categories.
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 2 36 And 2 86 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets
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Author :
language : en
Publisher:
Release Date : 1963
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 2 36 And 2 86 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets written by 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.
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 20 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets
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Author :
language : en
Publisher:
Release Date : 1963
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 20 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets written by 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.
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Number Of 1 41 And 2 20 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets
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Author : Gerald V. Foster
language : en
Publisher:
Release Date : 1963
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Number Of 1 41 And 2 20 Of A Variable Sweep Airplane Configuration Having Vertical Ramp Inlets written by Gerald V. Foster 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.
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 20 Of A Variable Sweep Airplane Configuration Having Body Mounted Nacelles With Conical Inlets
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Author :
language : en
Publisher:
Release Date : 1963
Static Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers Of 1 41 And 2 20 Of A Variable Sweep Airplane Configuration Having Body Mounted Nacelles With Conical Inlets written by 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.
Static Longitudinal And Lateral Aerodynamic Characteristic At A Mach Number Of 2 20 Of A Variable Sweep Fighter Airplane Configuration Having Body Mounted Nacelles With Vertical Ramp Inlets
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Author :
language : en
Publisher:
Release Date : 1963
Static Longitudinal And Lateral Aerodynamic Characteristic At A Mach Number Of 2 20 Of A Variable Sweep Fighter Airplane Configuration Having Body Mounted Nacelles With Vertical Ramp Inlets written by 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.
Static Longitudinal And Lateral Aerodynamic Characteristics At A Mach Number Of 2 20 Of A Variable Wing Sweep Stol Configuration
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Author : Gerald V. Foster
language : en
Publisher:
Release Date : 1960
Static Longitudinal And Lateral Aerodynamic Characteristics At A Mach Number Of 2 20 Of A Variable Wing Sweep Stol Configuration written by Gerald V. Foster 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.
Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers From 0 60 To 4 63 For Two Variable Sweep Configurations
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Author :
language : en
Publisher:
Release Date : 1965
Longitudinal And Lateral Aerodynamic Characteristics At Mach Numbers From 0 60 To 4 63 For Two Variable Sweep Configurations written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.
Static Longitudinal And Lateral Aerodynamic Characteristics At A Mach Number Of 2 20 Of A V Stol Airplane Configuration With A Variable Sweep Wing And With A Skewed Wing Design
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Author : Odell A. Morris
language : en
Publisher:
Release Date : 1961
Static Longitudinal And Lateral Aerodynamic Characteristics At A Mach Number Of 2 20 Of A V Stol Airplane Configuration With A Variable Sweep Wing And With A Skewed Wing Design 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 1961 with Airplanes categories.
Investigation Of The Aerodynamic Characteristics In Pitch And Sideslip Of A 45 Swept Wing Airplane Configuration With Various Vertical Locations Of The Wing And Horizontal Tail
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1957
Investigation Of The Aerodynamic Characteristics In Pitch And Sideslip Of A 45 Swept Wing Airplane Configuration With Various Vertical Locations Of The Wing And Horizontal Tail written by M. Leroy Spearman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Airplanes categories.
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.