|
|
|
|
|
Polina Talalaeva, Konstantin Starostin and Roman Savelyev
In this article, a calculation model for a fuel system of a light helicopter was developed for experimental and operational testing. The model analyzes the operation of not only the units, but also the whole fuel system, offering the basis for functional...
ver más
|
|
|
|
|
|
|
|
|
|
|
Kirill S. Anisimov,Andrey A. Savelyev,Innocentiy A. Kursakov,Alexander V. Lysenkov,Prajwal S. Prakasha
Pág. 93 - 97
Nacelle shape optimization for Blended Wing Body (BWB) is performed. The optimization procedure is based on numerical calculations of the Reynolds?averaged Navier?Stokes equations. For the Top Level Aircraft Requirements, formulated in AGILE project, the...
ver más
|
|
|
|
|
|
|
|
|
|
|
Yarovoy, A.G.; Savelyev, T.G.; Aubry, P.J.; Lys, P.E.; Ligthart, L.
Pág. 1288 - 1295
|
|
|
|
|
|