Avionics Specialties in partnership with Honeywell has developed an integra
ted ail data pressure sensor known as the integrated multi-function probe (
IMFP). This continuously flow-aligned pressure-sensing device was developed
using a multidisciplinary design approach encompassing computational fluid
dynamic, (CFD), flow analysis, and experimentation. The computational inve
stigation was performed using the finite clement code, CFDesign, by Blue Ri
dge Numerics and consisted of pressure distribution studies for varying flo
ws around conical sections. The application and integration of tills techno
logy to previously developed now alignment a,ld pressure transducing produc
ts lead to design similarity analysis saving considerable development time.
Initial experimentation used to develop and refine the design and analysis
consisted of laboratory bench testing, low and high-speed wind tunnel inve
stigations, and subsonic flight-testing. Final performance verification was
accomplished through data reduction and analysis of an extensive night tes
t program using a Lockheed Martin F-16 Fighting Falcon. The analysis, desig
n and performance verification of this innovative pressure-sensing device w
as investigated for direct comparison to conventional Pitot-static performa
nce with particular emphasis toward military fighter aircraft applications.