Author: Kalman J. GrunwaldPublisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 84
Book Description
Experimental Investigation of the Use of Slotted Test-section Walls to Reduce Wall Interference for High-lift-model Testing
Author: Kalman J. GrunwaldPublisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 84
Book Description
NASA Technical Note
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 536
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 464
Book Description
NASA Technical Memorandum
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64
Book Description
Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1478
Book Description
Applied Mechanics Reviews
Author: Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 300
Book Description
Analytical Study of Ventilated Wind Tunnel Boundary Interference on V/STOL Models Including Wake Curvature and Decay Effects
Author: E. M. KraftPublisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 74
Book Description
The wind tunnel boundary interference on a V/STOL model is calculated in a rectangular test section with solid vertical walls and ventilated (perforated or slotted) horizontal walls. The interference is found by applying the small perturbation theory of an incompressible fluid to the boundary value problem. The theory uses an image method in addition to Fourier transforms with an equivalent homogeneous boundary condition on the ventilated wall. The mathematical representation of the V/STOL model accounts for the curvature and decay of the wake. The assumption of a constant wake strength produces a paradox in that the maximum value of the interference factors increases as the initial jet velocity decreases. The most significant aspect of the analysis shows that nonlinear cross-flow effects at the tunnel boundary are important in the V/STOL case, and a quasi-linear approximation to these effects is introduced into the solution providing good agreement with experimental data.
NASA Technical Paper
Author: Publisher:
ISBN:
Category : Science
Languages : en
Pages : 88
Book Description
NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 350
Book Description
Report
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 430
Book Description
