Aerodynamic Characteristics Of A Canard Balanced Free Floating All Movable Stabilizer As Obtained From Rocket Powered Model Flight Tests And Low Speed Wind Tunnel Tests
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Aerodynamic Characteristics Of A Canard Balanced Free Floating All Movable Stabilizer As Obtained From Rocket Powered Model Flight Tests And Low Speed Wind Tunnel Tests
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Author : William N. Gardner
language : en
Publisher:
Release Date : 1953
Aerodynamic Characteristics Of A Canard Balanced Free Floating All Movable Stabilizer As Obtained From Rocket Powered Model Flight Tests And Low Speed Wind Tunnel Tests written by William N. Gardner 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.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1954
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.
Research Abstracts And Reclassification Notice
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Research Abstracts And Reclassification Notice written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.
Wadc Technical Report
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Author : United States. Wright Air Development Division
language : en
Publisher:
Release Date : 1957
Wadc Technical Report written by United States. Wright Air Development Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
A New Dimension Wallops Island Flight Test Range
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Author : Joseph Adams Shortal
language : en
Publisher:
Release Date : 1978
A New Dimension Wallops Island Flight Test Range written by Joseph Adams Shortal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Aeronautics categories.
Subject Index To Unclassified Astia Documents
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1960
Subject Index To Unclassified Astia Documents written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Industrial arts categories.
Low Speed Static Lateral Stability Characteristics Of A Canard Model Having A 60 Triangular Wing And Horizontal Tail
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Author : William R. Bates
language : en
Publisher:
Release Date : 1949
Low Speed Static Lateral Stability Characteristics Of A Canard Model Having A 60 Triangular Wing And Horizontal Tail written by William R. Bates and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Airplanes categories.
Correlation Of Aerodynamic Stability And Control Derivatives Obtained From Flight Tests And Wind Tunnel Tests On The Xc 142a Airplane
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Author : Ernest L. Black
language : en
Publisher:
Release Date : 1969
Correlation Of Aerodynamic Stability And Control Derivatives Obtained From Flight Tests And Wind Tunnel Tests On The Xc 142a Airplane written by Ernest L. Black and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamics categories.
Estimated Static Stability And Control Characteristics
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Author : GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED ENGINE AND TECHNOLOGY Dept
language : en
Publisher:
Release Date : 1964
Estimated Static Stability And Control Characteristics written by GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED ENGINE AND TECHNOLOGY Dept and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
The XV-5A is a two-engine, two-place V/STOL research aircraft with a design gross weight of 9200 pounds and an aspect ratio 3.42 wing of 260 square feet. In conventional flight mode the aircraft has a power-off flaps-down stall speed of 89 knots and a design maximum speed of 450 knots. In fan flight mode the aircraft can sustain flight at any speed from hovering to speeds in excess of conventional stall speed. The report represents an estimate the XV-5A aerodynamic characteristics, based on theoretical and empirical considerations, including the results of 420 hours of wind tunnel tests of 1/8 and 1/6 scale models. In the fan flight mode, the aircraft is estimated to be statically unstable in pitch with the most aft cg at low speeds below approximately 70 knots but with an increasing stability with speed to the conversion speed where the stability level corresponds to that for conventional flight. The aircraft possesses positive lateral and directional static stability with sideslip at all forward speeds in fan-powered flight and the effectiveness of the conventional flight control system is shown to be unaffected by fan operation. The exit louver control system is capable of providing the required propulsive force for acceleration of the airplane from a minimum of 10 knots rearward to conversion speed and provides a thrust attenuation of up to 22% for hovering lift control. (Author).