Author: Bernd Chudoba
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
A Project Method for Calculating Spanwise Lift Distributions on Swept and Unswept Wings at Subsonic Speeds
Calculated Spanwise Lift Distributions, Influence Functions, and Influence Coefficients for Unswept Wings in Subsonic Flow
Author: Franklin W. Diederich
Publisher:
ISBN:
Category :
Languages : en
Pages : 120
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 120
Book Description
A Finite-step Method for Estimating the Spanwise Lift Distribution of Wings in Symmetric, Yawed, and Rotary Flight at Low Speeds
The Calculation of Span Load Distributions on Swept-back Wings
Author: William Mutterperl
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description
Span load distributions of swept-back wings have been calculated. The method used was to replace the wing with a bound vortex at the quarter-chord line and to calculate the downwash due to the system of bound and trailing vortices to conform at the three-quarter-chord line to the slope of the flat-plate wing surface. Results are given for constant-chord and 5:1 tapered plan forms, for swee-pback angles of 0, 30 and 45 degresss, and for aspect ratios of 3, 6, and 9. Some comments on the stalling of swept-back wings are included.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description
Span load distributions of swept-back wings have been calculated. The method used was to replace the wing with a bound vortex at the quarter-chord line and to calculate the downwash due to the system of bound and trailing vortices to conform at the three-quarter-chord line to the slope of the flat-plate wing surface. Results are given for constant-chord and 5:1 tapered plan forms, for swee-pback angles of 0, 30 and 45 degresss, and for aspect ratios of 3, 6, and 9. Some comments on the stalling of swept-back wings are included.
Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings
Author: Almer D. Crim
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 344
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 344
Book Description
A Simple Approximate Method for Obtaining Spanwise Lift Distributions Over Swept Wings
Author: Franklin W. Diederich
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 58
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 58
Book Description
Scientific and Technical Aerospace Reports
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1246
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1246
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138
Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138
Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.