The Effects Of Wing Vertical Location And Vertical Tail Arrangement On The Stability Characteristics Of Canard Airplane Configurations Having Delta And Trapezoidal Planforms At Mach Numbers From 2 38 To 4 00
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The Effects Of Wing Vertical Location And Vertical Tail Arrangement On The Stability Characteristics Of Canard Airplane Configurations Having Delta And Trapezoidal Planforms At Mach Numbers From 2 38 To 4 00
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Author : Frank H. Jr Nichols
language : en
Publisher:
Release Date : 1961
The Effects Of Wing Vertical Location And Vertical Tail Arrangement On The Stability Characteristics Of Canard Airplane Configurations Having Delta And Trapezoidal Planforms At Mach Numbers From 2 38 To 4 00 written by Frank H. Jr Nichols 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.
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.
Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Delta Wing
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Author : Cornelius Driver
language : en
Publisher:
Release Date : 1960
Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Delta Wing 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 1960 with Airplanes categories.
Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Deg Delta Wing
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Author :
language : en
Publisher:
Release Date : 1960
Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Deg Delta Wing 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.
Effects Of Wing Vertical Location On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A Trapezoidal Aspect Ratio 3 Wing
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Author : Gerald V. Foster
language : en
Publisher:
Release Date : 1959
Effects Of Wing Vertical Location On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A Trapezoidal Aspect Ratio 3 Wing 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 1959 with Aerodynamics, Supersonic categories.
Investigation At High Subsonic Speeds Of The Static Longitudinal And Lateral Stability Characteristics Of Two Canard Airplane Configurations
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Author : William C. Steeman
language : en
Publisher: BiblioGov
Release Date : 2013-07
Investigation At High Subsonic Speeds Of The Static Longitudinal And Lateral Stability Characteristics Of Two Canard Airplane Configurations written by William C. Steeman and has been published by BiblioGov this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-07 with categories.
The present investigation was conducted in the Langley high-speed 7-by 10-foot tunnel to determine the static longitudinal and lateral stability characteristics at high subsonic speeds of two canard airplane configurations previously tested at supersonic speeds. The Mach number range of this investigation extended from 0.60 to 0.94 and a maximum angle-of-attack range of -2dewg to 24deg was obtained at the lowest test Mach number. Two wing plan forms of equal area were studied in the present tests; one was a 60deg delta wing and the other was a trapezoid wing having an aspect ratio of 3, taper ratio of 0.143, and an unswept 80-percent-chord line. The canard control had a trapezoidal plan form and its area was approximately 11.5 percent of the wing area. The model also had a low-aspect-ratio highly swept vertical tail and twin ventral fins. The longitudinal control characteristics of the models were consistent with past experience at low speed on canard configurations in that stalling of the canard surface occurred at moderate and high control deflections for moderate values of angle of attack. This stalling could impose appreciable limitations on the maximum trim-lift coefficient attainable. The control effectiveness and maximum value of trim-lift was significantly increased by addition of a body flap having a conical shape and located slightly behind the canard surface on the bottom of the body. Addition of the canard surface at 0deg deflection had relatively little effect on overall directional stability of the delta-wing configuration; however, deflection of the canard surface from 0deg to 10deg had a large favorable effect on directional stability at high angles of attack for both the trapezoid- and delta-wing configurations.
Effects Of Forebody Length On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A Trapezoidal Aspect Ratio 3 Wing
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1962
Effects Of Forebody Length On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A Trapezoidal Aspect Ratio 3 Wing 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 1962 with Airplanes categories.
Effects Of Wing Vertical Location On Stability And Control Characteristics At Mach Number Of 2 01 Of Canard Airplane Configuration With Trapezoidal Aspect Ratio 3 Wing With List Of References
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Author :
language : en
Publisher:
Release Date : 1959
Effects Of Wing Vertical Location On Stability And Control Characteristics At Mach Number Of 2 01 Of Canard Airplane Configuration With Trapezoidal Aspect Ratio 3 Wing With List Of References 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.
Effects Of Configuration Geometry On The Transonic Aerodynamic Characteristics Of Canard Airplane Configurations
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Author : James A. Blackwell (Jr.)
language : en
Publisher:
Release Date : 1964
Effects Of Configuration Geometry On The Transonic Aerodynamic Characteristics Of Canard Airplane Configurations written by James A. Blackwell (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerodynamics, Transonic categories.
Effects Of Forebody Length On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A Trapezoidal Aspect Ratio 3 Wing
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1962
Effects Of Forebody Length On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A Trapezoidal Aspect Ratio 3 Wing 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 1962 with categories.
A study was conducted in the Langley 4- by 4-foot supersonic pressure tunnel at a Mach number of 2.01 to determine the stability and control characteristics of a canard airplane configuration equipped with a trapez i al aspect-ratio-3 wing. Three bodies having length-diameter ratios of 9.45, 11.1, and 12.5 were investigated. The ratio of canard exposed area to wing total area was 0.0707. The model was equipped with a single, swept, body-mounted vertical tail. The experimentally determined variations of control effectiveness and longitudinal stability parameter wit canard volume were in reasonably close agreement with estimated variations. As the body length increased, the maximum trimmed values of lift-drag ratio L/D decreased at low stability levels and increased at high stability levels. At low angles of attack, directional stability decreased with increasing body length. With increasing angle of attack, an additional decrease in directi nal stability occurred because of a decrease in tail contribution which became progressively worse as the body length increased. (Author).