[PDF][PDF] Fitting fitness in aircraft design
WJ Vankan, R Maas, M Laban - 2006 - reports.nlr.nl
… meta-model many different fitting methods are available (eg [… of different fitting methods are
applied to aircraft design … of Design Of Experiments (DOE) methods. In the selected sample …
applied to aircraft design … of Design Of Experiments (DOE) methods. In the selected sample …
[图书][B] Aircraft performance
M Saarlas - 2006 - books.google.com
… limitations of various classes of aircraft is needed to establish … with the methods by which the
performance of an aircraft can be … However, such a design iteration procedure is outside the …
performance of an aircraft can be … However, such a design iteration procedure is outside the …
A feature-based automatic broken surfaces fitting method for complex aircraft skin parts
G Zhou, Y Li, C Liu, X Hao - The International Journal of Advanced …, 2016 - Springer
… fitting of aircraft … fitting method which can meet process requirements is desperately needed.
In this paper, a feature-based automatic fitting method for broken surfaces of complex aircraft …
In this paper, a feature-based automatic fitting method for broken surfaces of complex aircraft …
Aircraft design optimization
… At the near-field plane location, the pressure signature created by the aircraft is extracted
and propagated down to the ground using extrapolation methods based on geometric acoustics…
and propagated down to the ground using extrapolation methods based on geometric acoustics…
" Fuel Flow Method2" for Estimating Aircraft Emissions
D DuBois, GC Paynter - Sae Transactions, 2006 - JSTOR
… APPLYING ICAO DATABANK CURVE FIT (4 pt Method) With this logarithmic fit of 4 ICAO
data points (which we will call the 4 pt method) we can return to the same modern turbofan …
data points (which we will call the 4 pt method) we can return to the same modern turbofan …
Aircraft configuration optimization including optimized flight profiles
LA McCullers - NASA. Langley Research Center Recent Experiences …, 1984 - ntrs.nasa.gov
… Fighter weight equations were developed using a data base of 22 recent fighter and attack
aircraft. The transport data base included aircraft from the T-39 Sabreliner to the Boeing 747. …
aircraft. The transport data base included aircraft from the T-39 Sabreliner to the Boeing 747. …
A Superior Method of Installing Aircraft Fittings and Hardware
L Reid - 2006 - sae.org
… method of installing aerospace fittings and … fitting system provides a fast and robust installation
process that reduces both cost and assembly complexity compared to traditional methods, …
process that reduces both cost and assembly complexity compared to traditional methods, …
[HTML][HTML] A review on aircraft spectra simplification techniques for composite structures
… consuming process and a necessary part of certification for aircraft … Hence it is more pertinent
to develop effective methods for … techniques mainly include a spectrum truncation method …
to develop effective methods for … techniques mainly include a spectrum truncation method …
System identification for small, low-cost, fixed-wing unmanned aircraft
A Dorobantu, A Murch, B Mettler, G Balas - Journal of Aircraft, 2013 - arc.aiaa.org
… This paper describes a practical system identification procedure for small, low-cost, fixed-wing
unmanned aircraft. Physical size and cost restrictions limit the sensing capabilities of …
unmanned aircraft. Physical size and cost restrictions limit the sensing capabilities of …
Using big-data and surface fitting to improve aircraft safety through the study of relationships and anomalies
D Wooder, A Purvis, R McWilliam - Procedia CIRP, 2017 - Elsevier
… being fitted to (This method is referred to in this paper as Method … direction of the fitted function
over the x, y plane in consideration … (This method is referred to in this paper as Method B). …
over the x, y plane in consideration … (This method is referred to in this paper as Method B). …