Results 41 to 50 of about 10,561 (136)

Finite element analysis of low speed viscous and inviscid aerodynamic flows [PDF]

open access: yes
A weak interaction solution algorithm was established for aerodynamic flow about an isolated airfoil. Finite element numerical methodology was applied to solution of each of differential equations governing potential flow, and viscous and turbulent ...
Baker, A. J., Manhardt, P. D.
core   +1 more source

On the positivity of fvs schemes [PDF]

open access: yes, 1999
Over the last ten years, robustness of schemes has raised an increasing interest among the CFD community. One mathematical aspect of scheme robustness is the positivity preserving property.
Gressier, Jérémie   +1 more
core  

Application of empirical and linear methods to VSTOL powered-lift aerodynamics [PDF]

open access: yes
Available prediction methods applied to problems of aero/propulsion interactions for short takeoff and vertical landing (STOVL) aircraft are critically reviewed and an assessment of their strengths and weaknesses provided.
Kuhn, Richard, Margason, Richard
core   +1 more source

Numerical and experimental study of aerosol dispersion in the Do728 aircraft cabin. [PDF]

open access: yesCEAS Aeronaut J, 2023
Schmeling D   +3 more
europepmc   +1 more source

Developments in steady and unsteady aerodynamics for use in aeroelastic analysis and design [PDF]

open access: yes
A review is given of seven research projects which are aimed at improving the generality, accuracy, and computational efficiency of steady and unsteady aerodynamic theory for use in aeroelastic analysis and design.
Bland, S. R., Yates, E. C., Jr.
core   +1 more source

PAN AIR summary document (version 1.0) [PDF]

open access: yes
The capabilities and limitations of the panel aerodynamics (PAN AIR) computer program system are summarized. This program uses a higher order panel method to solve boundary value problems involving the Prandtl-Glauert equation for subsonic and supersonic
Derbyshire, T., Sidwell, K. W.
core   +1 more source

Unsteady aerodynamic analysis of space shuttle vehicles. Part 1: Summary report [PDF]

open access: yes
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show that slender wing theory can be modified to give the potential flow static and dynamic characteristics over a large Mach number range from M = 0 to M 1. A
Ericsson, L. E., Reding, J. P.
core   +1 more source

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