Author:
Tejero Fernando,Doerffer Piotr,Flaszyński Paweł,Szulc Oskar
Publisher
Springer International Publishing
Reference11 articles.
1. Ahmad J, Duque EPN (1996) Helicopter rotor blade computation in unsteady flows using moving overset grids. J Aircr 33(1):54–60
2. Boniface JC (2014) A computational framework for helicopter fuselage drag reduction using vortex generators. In: AHS 70th Annual Forum, Montreal, Canada
3. Caradonna FX, Tung C (1981) Experimental and analytical studies of a model helicopter rotor in hover. NASA Technical Memorandum 81232
4. Cross JL, Watts ME (1988) Tip aerodynamics and acoustics test. NASA Reference Publication 1179
5. Kang HJ, Kwon OJ (2002) Unstructured mesh Navier-Stokes calculations of the flow field of a helicopter rotor in hover. J Am Helicopter Soc 47(2):90–99