Clausen R.D. computational model for thickening boundary layers with mass addition for hypersonic engine inlet testing : Rep.presented at the AIAA/SAE/ASME/ASEE 26th joint propulsion conf.,July 16-18,1990 / R.D.Clausen,P.I.King, 1990. - 8 p. - Текст : непосредственный.
Galassi L. Effects of inlet turbulence scale on blade surface heat transfer in a linear Cascade : Rep.presented at AIAA/SAE/ASME/ASEE 26th joint propulsion conf.,July 16-18,1990,Orlando,Fl / L.Galassi,P.I.King,W.C.Elrod, 1990. - 12 p. - Текст : непосредственный.