Results 101 to 110 of about 21,634 (177)

Transonic airfoil design for helicopter rotor applications [PDF]

open access: yes
Despite the fact that the flow over a rotor blade is strongly influenced by locally three-dimensional and unsteady effects, practical experience has always demonstrated that substantial improvements in the aerodynamic performance can be gained by ...
Hassan, Ahmed A., Jackson, B.
core   +1 more source

TRANDESNF: A computer program for transonic airfoil design and analysis in nonuniform flow [PDF]

open access: yes
The use of a transonic airfoil code for analysis, inverse design, and direct optimization of an airfoil immersed in propfan slipstream is described. A summary of the theoretical method, program capabilities, input format, output variables, and program ...
Chang, J. F., Lan, C. Edward
core   +1 more source

Aerodynamics of an airfoil with a jet issuing from its surface [PDF]

open access: yes
A simple, two dimensional, incompressible and inviscid model for the problem posed by a two dimensional wing with a jet issuing from its lower surface is considered and a parametric analysis is carried out to observe how the aerodynamic characteristics ...
Karamcheti, K., Tavella, D. A.
core   +1 more source

Improvements to tilt rotor performance through passive blade twist control [PDF]

open access: yes
A passive blade twist control is presented in which the twist distribution of a tilt rotor blade is elastically changed as a function of rotor speed. The elastic twist deformation is used to achieve two different blade twist distributions corresponding ...
Nixon, Mark W.
core   +1 more source

On simple aerodynamic sensitivity derivatives for use in interdisciplinary optimization [PDF]

open access: yes
Low-aspect-ratio and piston aerodynamic theories are reviewed as to their use in developing aerodynamic sensitivity derivatives for use in multidisciplinary optimization applications.
Doggett, Robert V., Jr.
core   +1 more source

Optimization of Flapping Airfoils for Maximum Thrust and Propulsive Efficiency

open access: yesActa Polytechnica, 2004
A numerical optimization algorithm based on the steepest decent along the variation of the optimization function is implemented for maximizing the thrust and/or propulsive efficiency of a single flapping airfoil.
I. H. Tuncer, M. Kay
doaj  

Application of numerical optimization to the design of wings with specified pressure distributions [PDF]

open access: yes
A practical procedure for the optimum design of transonic wings is demonstrated. The procedure uses an optimization program based on the method of feasible directions coupled with an aerodynamic analysis program which solves the three-dimensional ...
Haney, H. P., Johnson, R. R.
core   +1 more source

CFD-enabled sustainable design and manufacturing of cooling fan for unmanned helicopter. [PDF]

open access: yesSci Rep
Si L   +10 more
europepmc   +1 more source

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