Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Degree Swept Wing At Mach Numbers From 0 80 To 0 98
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Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Degree Swept Wing At Mach Numbers From 0 80 To 0 98
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Author : F. E. West
language : en
Publisher:
Release Date : 1960
Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Degree Swept Wing At Mach Numbers From 0 80 To 0 98 written by F. E. West and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Deg Swept Wing At Mach Numbers From 0 80 To 0 98
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Author :
language : en
Publisher:
Release Date : 1960
Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Deg Swept Wing At Mach Numbers From 0 80 To 0 98 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Aero Digest Latino Americano Edic On
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Author : Eduardo Borda
language : es
Publisher:
Release Date : 1963
Aero Digest Latino Americano Edic On written by Eduardo Borda and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aeronautics categories.
Aerodynamic Characteristics Of A Spoiler Slot Deflector Control On A 45 Sweptback Wing At Mach Numbers Of 1 61 And 2 01
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Author : Douglas R. Lord
language : en
Publisher:
Release Date : 1957
Aerodynamic Characteristics Of A Spoiler Slot Deflector Control On A 45 Sweptback Wing At Mach Numbers Of 1 61 And 2 01 written by Douglas R. Lord and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamics categories.
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of a spoiler-slot-deflector control on a 45 degree sweptback wing having an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section. The model was equipped with a 15-percent-chord spoiler-slot-deflector extending from 13 o 78 percent of the wing semispan. The spoiler and deflector were hinged along the 60- and 75-percent-chord lines, respectively. Tests were made at a Reynolds number of 3,000,000 (based on the mean aerodynamic chord of the wing) and covered ranges of angles of attack from -3 to 15 degrees, spoiler projections from 0 to 8.0 percent chord, and deflector projections from 0 to 7.6 percent chord.
Investigation Of Spoiler Ailerons For Use As Speed Brakes Or Glide Path Controls On Two Naca 65 Series Wings Equipped With Full Span Slotted Flaps
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Author : Jack Fischel
language : en
Publisher:
Release Date : 1949
Investigation Of Spoiler Ailerons For Use As Speed Brakes Or Glide Path Controls On Two Naca 65 Series Wings Equipped With Full Span Slotted Flaps written by Jack Fischel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerofoils categories.
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency operatiion of airplanes. These speed brakes or glide-path controls would probably have small effect on wing pitching moments and should retain their rolling effectiveness.
An Investigation Of The Drag Characteristics Of Speed Brakes For Mach Numbers From 0 20 To 1 30
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Author : Allan R. Vick
language : en
Publisher:
Release Date : 1958
An Investigation Of The Drag Characteristics Of Speed Brakes For Mach Numbers From 0 20 To 1 30 written by Allan R. Vick and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Airplanes categories.
Effects Of Wing Planform On The Aerodynamic Characteristics Of A Wing Body Tail Model At Mach Numbers 1 57 2 16 And 2 87
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Author :
language : en
Publisher:
Release Date : 1965
Effects Of Wing Planform On The Aerodynamic Characteristics Of A Wing Body Tail Model At Mach Numbers 1 57 2 16 And 2 87 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.
Performance Stability And Control Investigation At Mach Numbers From 0 4 To 0 9 Of A Model Of The Swallow With Outer Wing Panels Swept 25 Degree With And Without Power Simulation
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Author :
language : en
Publisher:
Release Date : 1960
Performance Stability And Control Investigation At Mach Numbers From 0 4 To 0 9 Of A Model Of The Swallow With Outer Wing Panels Swept 25 Degree With And Without Power Simulation written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Beyond Tube And Wing
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Author : Bruce Larrimer
language : en
Publisher:
Release Date : 2020-06-15
Beyond Tube And Wing written by Bruce Larrimer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2020-06-15 with categories.
Popular Mechanics
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language : en
Publisher:
Release Date : 2000-01
Popular Mechanics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000-01 with categories.
Popular Mechanics inspires, instructs and influences readers to help them master the modern world. Whether it’s practical DIY home-improvement tips, gadgets and digital technology, information on the newest cars or the latest breakthroughs in science -- PM is the ultimate guide to our high-tech lifestyle.