Author: William R. BatesPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
Book Description
Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail
Author: William R. BatesPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
Book Description
Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail
Author: William R. BatesPublisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Low-speed Static Lateral-stabilty Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail
Author: William R. BatesPublisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface
Author: John W. DraperPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 43
Book Description
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 Stability Characteristics of a Cambered-delta-wing Model
Author: John M. RiebePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation was made in the Langley 300 MPH 7- by 10-foot tunnel to determine the static stability characteristics of a cambered-delta-wing model. The cambered delta wing was derived from a segment of a cone selected so that the projected plan form with a wing dihedral angle of zero degrees was the same as a 60 degree delta wing. The projected plan form had an aspect ratio of 2.31.
The Low-speed Static Longitudinal and Lateral Characteristics of a Delta-wing Model with Fixed and Free-floating Canard Surfaces
Author: William I. ScallionPublisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 64
Book Description
Low-speed Investigation of Effects of Vertical Tails on the Static Stability Characteristics of a Canard-bomber Configuration Having a Very Thin Wing and a Slender Elliptical Fuselage
Author: Thomas G. GainerPublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 24
Book Description
Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces
Author: Clarence D. Cone (Jr.)Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Book Description
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.
