Author: Harold Mirels
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
Book Description
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.
Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9
Author: Harold Mirels
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
Book Description
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
Book Description
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.
Experimental Determination of the Pressure Distribution on a Rectangular Wing Oscillating in the First Bending Mode for Mach Numbers from 0.24 to 1.30
Author: Henry C. Lessing
Publisher:
ISBN:
Category : Aerodynamics, aircraft
Languages : en
Pages : 98
Book Description
Publisher:
ISBN:
Category : Aerodynamics, aircraft
Languages : en
Pages : 98
Book Description
An Experimental Pressure-distribution Investigation of Interference Effects Produced at a Mach Number of 3.11 by Wedge- Shaped Bodies Located Under a Triangular Wing
Author: Lowell E. Hasel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 120
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 120
Book Description
Scientific and Technical Aerospace Reports
Scientific and Technical Aerospace Reports
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
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 : 666
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
Book Description
Index of NASA Technical Publications
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description