Results 71 to 80 of about 13,340 (180)

Unsteady supersonic aerodynamic theory for interfering surfaces by the method of potential gradient [PDF]

open access: yes
A generalized solution of the hyperbolic wave equation was further developed to relate the velocity components at a field point to the potential gradient distribution in the dependence domain.
Arppa, K., Jones, W. P.
core   +1 more source

Special opportunities in helicopter aerodynamics [PDF]

open access: yes
Aerodynamic research relating to modern helicopters includes the study of three dimensional, unsteady, nonlinear flow fields. A selective review is made of some of the phenomenon that hamper the development of satisfactory engineering prediction ...
Mccroskey, W. J.
core   +1 more source

Predicting wind turbine blade loads using vorticity transport and RANS methodologies [PDF]

open access: yes, 2009
Two computational methods, one based on the solution of the vorticity transport equation, and a second based on the solution of the Reynolds-Averaged Navier-Stokes equations, have been used to simulate the aerodynamic performance of a horizontal axis ...
Brown, Richard   +3 more
core  

Comparisons of several aerodynamic methods for application to dynamic loads analyses [PDF]

open access: yes
The results of a study are presented in which the applicability at subsonic speeds of several aerodynamic methods for predicting dynamic gust loads on aircraft, including active control systems, was examined and compared. These aerodynamic methods varied
Kroll, R. I., Miller, R. D.
core   +1 more source

Some effects of tip fins on wing flutter characteristics [PDF]

open access: yes
A wind tunnel investigation has been conducted over the Mach number range from about 0.6 to 1.2 to determine the effects of large tip fins on the flutter characteristics of a swept wing.
Doggett, R. V., Jr., Goetz, R. C.
core   +1 more source

Correlation of Puma airloads: Evaluation of CFD prediction methods [PDF]

open access: yes
A cooperative program was undertaken by research organizations in England, France, Australia and the U.S. to study the capabilities of computational fluid dynamics codes (CFD) to predict the aerodynamic loading on helicopter rotor blades.
Desopper, Andre   +3 more
core   +1 more source

Asymptotic Expansion of the Kernel Function in Subsonic Unsteady Lifting Surface Theory

open access: yesAsymptotic Expansion of the Kernel Function in Subsonic Unsteady Lifting Surface Theory
A computer oriented asymptotic expansion of a singular integral function is presented. The function dealt with appears in the kemel of the integral equation which is solved for pressure distributions of subsonic unsteady lifting surfaces. Values of the function can be accurately computed in a short time by using the present expansion.
openaire  

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