Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section
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Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics, Transonic categories.
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Having A 45 Degree Swept Wing Of Aspect Ratio 6 0
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Author : John C. McFall
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Having A 45 Degree Swept Wing Of Aspect Ratio 6 0 written by John C. McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamic load categories.
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Swept Wing Of Aspect Ratio 6 0
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Author : John C. Jr McFall
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Swept Wing Of Aspect Ratio 6 0 written by John C. Jr McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with categories.
Longitudinal Stability And Control Characteristics At Transonic Speeds Of A Semispan Airplane Model Having A 45 Degrees Sweptback Wing And Tail As Obtained By The Transonic Bump Method
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1948
Longitudinal Stability And Control Characteristics At Transonic Speeds Of A Semispan Airplane Model Having A 45 Degrees Sweptback Wing And Tail As Obtained By The Transonic Bump Method 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 1948 with categories.
Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degree Sweptback Wing And A Triangular All Movable Control Surface
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Author : Harold L. Crane
language : en
Publisher:
Release Date : 1950
Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degree Sweptback Wing And A Triangular All Movable Control Surface written by Harold L. Crane and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerofoils categories.
Measurements of the longitudinal stability and control characteristics of a canard airplane configuration have been made by the wing-flow method. The distinguishing features of this configuration in addition to the unconventional wing-stabilizer arrangement are the triangular plan form of the all-movable longitudinal control surface, the 45 degree sweptback wing of aspect ratio 4.1, and the slender body of fineness ratio 13.5. The investigation included measurements of lift, pitching moment, and rolling moment of the semispan model, with control settings between -4 degrees and 16 degrees and with the control surface removed. In some cases the angle-of-attack range was as great as from approximately -10 to 30 degrees. Approximate measurements of chord force were made at one stabilizer incidence. The Mach number range covered was from 0.55 to 1.14 at Reynolds numbers of the order of 400,000.
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.
Investigation Of Static Longitudinal Stability Characteristics At Transonic Speeds Of 30 Degree Sweptback Wing In Wing Body Configuration With And Without Horizontal Tail
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Author : Conrad M. Willis
language : en
Publisher:
Release Date : 1957
Investigation Of Static Longitudinal Stability Characteristics At Transonic Speeds Of 30 Degree Sweptback Wing In Wing Body Configuration With And Without Horizontal Tail written by Conrad M. Willis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with categories.
Longitudinal Stability And Control Characteristics Of A Semispan Airplane Model With A Swept Back Tail From Tests At Transonic Speeds By The Naca Wing Flow Method
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Author : John A. Zalovcik
language : en
Publisher:
Release Date : 1947
Longitudinal Stability And Control Characteristics Of A Semispan Airplane Model With A Swept Back Tail From Tests At Transonic Speeds By The Naca Wing Flow Method written by John A. Zalovcik and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aerodynamics, Transonic categories.
An investigation was made by the NACA wing-flow method to determine the longitudinal stability and control characteristics at transonic speeds of a semispan airplane model having a wing of conventional plan form and a horizontal tail swept back 45 degrees. The wing and tail had NACA 65-series airfoil sections with thicknesses of 10 and 8 percent chord, respectively. The model was mounted in such a way as to permit it to assume a position of zero pitching moment about a center of gravity at 27 percent of the mean aerodynamic chord. Measurements were made of lift and angle of attack for trim for several stabilizer and elevator settings.
Aerodynamic Characteristics At Transonic Speeds Of A Wing Having 45 Degrees Sweep Aspect Ratio 8 Taper Ratio 0 45 And Airfoil Sections Varying From The Naca 63a010 Section At The Root To The Naca 63a006 Section At The Tip
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Author : William D. Jr Morrison
language : en
Publisher:
Release Date : 1952
Aerodynamic Characteristics At Transonic Speeds Of A Wing Having 45 Degrees Sweep Aspect Ratio 8 Taper Ratio 0 45 And Airfoil Sections Varying From The Naca 63a010 Section At The Root To The Naca 63a006 Section At The Tip written by William D. Jr Morrison and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.