Results 71 to 80 of about 13,317 (179)

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.
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Calculation of unsteady transonic aerodynamics for oscillating wings with thickness [PDF]

open access: yes
An analytical approach is presented to account for some of the nonlinear characteristics of the transonic flow equation for finite thickness wings undergoing harmonic oscillation at sonic flight speed in an inviscid, shock-free fluid.
Ruo, S. Y., Theisen, J. G.
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Application of theory to propeller design [PDF]

open access: yes
The various theories concerning propeller design are discussed. The use of digital computers to obtain specific blade shapes to meet appropriate flow conditions is emphasized. The development of lifting-line and lifting surface configurations is analyzed.
Cox, G. G., Morgan, W. B.
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An integrated approach to the optimum design of actively controlled composite wings [PDF]

open access: yes
The importance of interactions among the various disciplines in airplane wing design has been recognized for quite some time. With the introduction of high gain, high authority control systems and the design of thin, flexible, lightweight composite wings,
Livne, E.
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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.
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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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