Static Longitudinal Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 41 1 61 And 2 01
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Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07
Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1987
Government Reports Announcements 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 1987 with Government publications categories.
Static Longitudinal Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 41 1 61 And 2 01
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Author : Cornelius Driver
language : en
Publisher:
Release Date : 1956
Static Longitudinal Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 41 1 61 And 2 01 written by Cornelius Driver 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, Supersonic categories.
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the static longitudinal stability and control characteristics of a model of a 45 degrees swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01.
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1956
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01 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 1956 with categories.
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1956
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01 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 1956 with Airplanes categories.
Static Longitudinal And Lateral Stability And Control Characteristics Of A Model Of A 35 Degree Swept Wing Airplane At A Mach Number Of 1 41
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Author : Edward B. Palazzo
language : en
Publisher:
Release Date : 1955
Static Longitudinal And Lateral Stability And Control Characteristics Of A Model Of A 35 Degree Swept Wing Airplane At A Mach Number Of 1 41 written by Edward B. Palazzo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with categories.
Effects Of External Stores On The Static Longitudinal Aerodynamic Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 61 And 2 01
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Author : Gerald V. Foster
language : en
Publisher:
Release Date : 1956
Effects Of External Stores On The Static Longitudinal Aerodynamic Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 61 And 2 01 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 1956 with Airplanes categories.
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various external-store configurations of the longitudinal and lateral aerodynamic characteristics of a model of a 45 degree swept-wing fighter airplane. Pylon-mounted stores located at 23.8, 46.2, and 67.0 percent of the wing semispan were tested individually and in various combinations. The inboard stores relative to outboard stores were similar in shape but approximately 25 percent greater in size. The stores located at 46.2 percent of the wing semispan represented a large fuel tank and had an unsymmetrical shape.
Longitudinal Stability And Control Characteristics At Mach Numbers Of 1 41 And 2 01 Of A 67 Degree Swept Wing Airplane Configuration With Canard Control Surfaces
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1958
Longitudinal Stability And Control Characteristics At Mach Numbers Of 1 41 And 2 01 Of A 67 Degree Swept Wing Airplane Configuration With Canard Control Surfaces 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 1958 with categories.
Longitudinal Stability And Control Characteristics Of A Two Place All Weather Fighter Airplane Between Mach Numbers Of 0 80 And 2 00 Obtained From The Flight Test Of A Rocket Boosted Model
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Author :
language : en
Publisher:
Release Date : 1959
Longitudinal Stability And Control Characteristics Of A Two Place All Weather Fighter Airplane Between Mach Numbers Of 0 80 And 2 00 Obtained From The Flight Test Of A Rocket Boosted Model written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
Static Longitudinal Stability And Control Characteristics Of A 1 16 Scale Model Of The Douglas D 558 Ii Research Airplane At Mach Numbers Of 1 61 And 2 01
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1953
Static Longitudinal Stability And Control Characteristics Of A 1 16 Scale Model Of The Douglas D 558 Ii Research Airplane At Mach Numbers Of 1 61 And 2 01 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 1953 with categories.