Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail
Title | Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF eBook |
Author | William R. Bates |
Publisher | |
Pages | 16 |
Release | 1949 |
Genre | |
ISBN |
Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail
Title | Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail PDF eBook |
Author | William R. Bates |
Publisher | |
Pages | 38 |
Release | 1949 |
Genre | Airplanes |
ISBN |
Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface
Title | Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface PDF eBook |
Author | John W. Draper |
Publisher | |
Pages | 43 |
Release | 1950 |
Genre | Aerofoils |
ISBN |
An investigation has been made of the low-speed static stability characteristics of a canard model with a 45 degree sweptback wing and a 60 degree triangular horizontal control surface. The model had practically no allowable center-of-gravity range because of longitudinal instability that occurred at moderate and high lift coefficients with horizontal-control-surface incidences of 10 degrees or less. The horizontal control surface produced a sidewash which, at an incidence of 15 degrees at angles of attack greater than 7 degrees, was strong enough to make the model directionally stable with the vertical tail off. This sidewash caused a vertical tail mounted on the fuselage to be destabilizing at angles of attack above 11 degrees. Twin vertical tails mounted at the wing tips did not produce a similar destabilizing effect because they were located outside the sidewash field.
Low-speed Static Lateral-stabilty Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail
Title | Low-speed Static Lateral-stabilty Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF eBook |
Author | William R. Bates |
Publisher | |
Pages | 29 |
Release | 1949 |
Genre | |
ISBN |
Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces
Title | Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces PDF eBook |
Author | Clarence D. Cone (Jr.) |
Publisher | |
Pages | 76 |
Release | 1959 |
Genre | Airplanes |
ISBN |
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 1008 |
Release | 1978 |
Genre | Aeronautics |
ISBN |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
The Low-speed Static Longitudinal and Lateral Characteristics of a Delta-wing Model with Fixed and Free-floating Canard Surfaces
Title | The Low-speed Static Longitudinal and Lateral Characteristics of a Delta-wing Model with Fixed and Free-floating Canard Surfaces PDF eBook |
Author | William I. Scallion |
Publisher | |
Pages | 64 |
Release | 1959 |
Genre | Delta wing airplanes |
ISBN |