Results 31 to 40 of about 10,561 (136)

Compressible unsteady potential aerodynamic flow around lifting bodies having arbitrary shapes and motions [PDF]

open access: yes
The program SUSSA ACTS, steady and unsteady subsonic and supersonic aerodynamics for aerospace complex transportation system, is presented. Fully unsteady aerodynamics is discussed first, followed by developments on normal wash, pressure distribution ...
Morino, L.
core   +1 more source

Leading-edge vortex research: Some nonplanar concepts and current challenges [PDF]

open access: yes
Some background information is provided for the Vortex Flow Aerodynamics Conference and that current slender wing airplanes do not use variable leading edge geometry to improve transonic drag polar is shown.
Campbell, J. F., Osborn, R. F.
core   +1 more source

Pseudo-shock waves and their interactions in high-speed intakes [PDF]

open access: yes, 2016
In an air-breathing engine the flow deceleration from supersonic to subsonic conditions takes places inside the isolator through a gradual compression consisting of a series of shock waves.
Gnani, F., Kontis, K., Zare-Behtash, H.
core   +1 more source

Wind tunnel wall interference (January 1980 - May 1988): A selected, annotated bibliography [PDF]

open access: yes
This selected bibliography lists 423 entries on the subject of wall interference during testing in wind tunnels. It is the third in a series of bibliographies on the subject.
Cole, Karen L., Tuttle, Marie H.
core   +1 more source

Aeronautical Engineering. A continuing bibliography, supplement 115 [PDF]

open access: yes
This bibliography lists 273 reports, articles, and other documents introduced into the NASA scientific and technical information system in October ...

core   +1 more source

A technique for accelerating iterative convergence in numerical integration, with application in transonic aerodynamics [PDF]

open access: yes
A technique is described for the efficient numerical solution of nonlinear partial differential equations by rapid iteration. In particular, a special approach is described for applying the Aitken acceleration formula (a simple Pade approximant) for ...
Martin, E. D.
core   +1 more source

A Green's function formulation for a nonlinear potential flow solution applicable to transonic flow [PDF]

open access: yes
Routine determination of inviscid subsonic flow fields about wing-body-tail configurations employing a Green's function approach for numerical solution of the perturbation velocity potential equation is successfully extended into the high subsonic ...
Baker, A. J., Fox, C. H., Jr.
core   +1 more source

The panel on propulsion aerodynamics [PDF]

open access: yes
Sources of discrepancies noted between propulsion aerodynamic characteristics as predicted from wind tunnel tests and as measured in flight are discussed.
Bowditch, D.
core   +1 more source

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