paolo.caccavale@gmail.com
info@fluere.it
paolo.caccavale@pec.fluere.it
PaMS
overview
intro
news
references
theory
user guide
test cases
applications
personal data &
educational training
work experience
academic activities
congresses &
publications
PaMS
Panel Method Solver
3D low-order unsteady Boundary Element Method for the solution of ideal flows (inviscid, incompressible and irrotational) with a numerical methodology based on the third Green’s Identity and the Morino’s formulation
...
news
2021: release to Sky Eye Systems
2020: release to Leonardo
2020: partnership with iBMB
2016-17: partecipation in Clean Sky 2
2016: partnership with Flowlab
2015: presentation to Move the Future
2012-13: demonstrator to ATR Toulouse
2008: release to CIRA
Previous
Next
test cases
cylinder
2D steady test case
thick non-lifting body
sphere
3D steady test case
thick non-lifting body, quad and tria mesh
NACA0012 airfoil
2D steady test case
“Dirichlet” boundary condition for thick lifting airfoils
NACA63 mean line
2D steady test case
“Neumann” boundary condition for thin lifting airfoil
elliptic wing
3D steady test case
lifting wing
oscill. flatplate
2D unsteady test case
oscillating thin lifting airfoil
oscillat. airfoil
2D unsteady test case
oscillating thick lifting airfoil
rotor hovering
3D unsteady test case
wake models
VAWT
3D unsteady test case
wake-body interference
NASA SR2 propeller
3D unsteady test case
wing-propeller configuration
tiltrotor
3D unsteady test case
wing-propeller configuration @ angle of attack up to 90deg
light aircraft
3D steady test case
wing-fuselage configuration
internal flow
3D steady test case
boundary conditions for internal flows
helicopter
3D unsteady test case
rotor-airframe aerodynamic interaction
Hi Lift PW-1
3D steady test case
slat-main-flap "Config. 1"
Hi Lift PW-2
3D steady test case
wing-body DLR F11 "Config. 4"
Previous
Next
applications
dolphin
tail fin (flukes) thrust evaluation
Rapier X-25
full UAS aerodynamics
PaMS vs OpenFOAM
military aircraft
propeller wake on the vertical and horizontal tail with lateral wind
light aircraft
effect of the propeller wakes on the wing lift distribution
flight refueling
effect of the tanker wake on the receiver lift distribution
business jet
rolling and heaving motion with lateral wind
stratofly
from the delta wing to the stratospheric flight
turboprop
propeller-wing wake on fuselage and vertical tail
UAV tiltrotor
unsteady aerodynamics (copter mode > tilt > plane mode) of a rough tiltrotor model
VAWT
effect of gust
HAWT
effect of the oscillating wind
CROR
aerodynamic analysis at typical sea-level take-off conditions
mini 6.50 hydro
hull hydrostatics and stability
mini 6.50 aero
aerodynamics of sails
aeroelasticity
PaMS-Nastran coupling
UAV joined wing
T-joint wake
car & bus
aerodynamic interference
dumned hunchback
historical aircraft
Previous
Next
amalfi
budapest
MAXXI museum
ferrari F1
MAXXI museum
minori
naxos
santorini
ischia
vento e vele
seagull
santorini
ischia
Fluere.it by Paolo Caccavale