[Reports] / Amer.inst.of aeronautics and astronautics. N 89-1850 : Inception length to a fully-developed fin-generated shock wave boundary-layer interaction : Rep. presented at AIAA 20th fluid dynamics, plasma dynamics a. lasers conf., Buffalo(NY), June 12-14, 1989 / F.Lu,G.Settles, 1989. - 11 p. - Текст : непосредственный.
Chung K. Shock-tube calibration of a fast-response pressure transducer : Paper presented at AIAA 16th aerodynamic ground testing conf.,June 18-20,1990,Seattle,Wa. / K.Chung,F.Lu, 1990. - 9 p. - Текст : непосредственный.