Author: Earl R. Keener
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Oil-flow Separation Patterns on an Ogive Forebody
Flow-separation Patterns on Symmetric Forebodies
Author: Earl R. Keener
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 148
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 148
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 376
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.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 376
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.
NASA Technical Memorandum
Mathematical Fluid Dynamic Modeling of Plasma Stall-spin Departure Control
Author: Norman D. Malmuth
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 36
Book Description
This report summarizes theoretical and CFD studies related to surface discharge to quench stall-slip departure due to asymmetric vortex shedding on aircraft nose tips, augment directional control/authority agility, and develop tailless capability. This approach offers adaptability in rapidly changing flight and mission conditions, constructional simplicity, massless operation, no changes in aerodynamic shape, no influence on aircraft characteristics when the system is not in use, and low weight and power penalties, and closed loop feedback control. In the first phase of the effort, lower-order theoretical modeling showed that vortex symmetry breakdown strongly depends on the boundary-layer separation locus. The latter can be effectively controlled by a surface discharge located upstream from the separation line. Using spark discharges of relatively small power (less than 1 kW) it is feasible to shift the separation line toward the windward surface and suppress vortex asymmetry.
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 36
Book Description
This report summarizes theoretical and CFD studies related to surface discharge to quench stall-slip departure due to asymmetric vortex shedding on aircraft nose tips, augment directional control/authority agility, and develop tailless capability. This approach offers adaptability in rapidly changing flight and mission conditions, constructional simplicity, massless operation, no changes in aerodynamic shape, no influence on aircraft characteristics when the system is not in use, and low weight and power penalties, and closed loop feedback control. In the first phase of the effort, lower-order theoretical modeling showed that vortex symmetry breakdown strongly depends on the boundary-layer separation locus. The latter can be effectively controlled by a surface discharge located upstream from the separation line. Using spark discharges of relatively small power (less than 1 kW) it is feasible to shift the separation line toward the windward surface and suppress vortex asymmetry.
Prediction of Vortex Shedding from Circular and Noncircular Bodies in Supersonic Flow
Author: M. R. Mendenhall
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 204
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 204
Book Description
Flow Visualization Techniques
Flow Visualization Techniques with Image Processing
Control of Submersible Vortex Flows
Author: D. M. Bushnell
Publisher:
ISBN:
Category : Submersibles
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Submersibles
Languages : en
Pages : 52
Book Description