Электронный каталог

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    Mach 6 testing of a scramjet engine model / T. Kanda, T. Saito, K. Kudoh, T. Komuro, 1998. - 20 p. - Текст : непосредственный.

    Mach 6 testing of a scramjet engine model / T. Kanda, T. Saito, K. Kudo, K. Tomoyuki, 1998. - 22 p. - Текст : непосредственный.

    Experimental studies of supersonic film cooling with shock wave interaction (II) / F. Ono, T. Kanda, T. Saito, Y. Wakamatsu, 1997. - 12 p. - Текст : непосредственный.

    Effect of regenerative cooling on rocket engine specific impulse / T. Kanda, G. Masuya, Y. Wakamatsu, A. Kanmuri, 1993. - 9 p. - Текст : непосредственный.

    [Reports] / Amer.inst.of aeronautics and astronautics. N 89-2736 : Transient analysis of LOX/LH2 rocket engine (LE-7) : Rep. presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf.,Monterey(Ca),July 10-12,1989 / A.Kanmuri,T.Kanda,Y.Wakamatsu и др, 1989. - 8 p. - Текст : непосредственный.

    comparison of scramjet engine performances of various cycles / T.Kanda,G.Masuya,Y.Wakamatsu и др., 1989. - 14 p. - Текст : непосредственный.

    Analysis of scramjet engine characteristics / T.Kanda,G.Masuya,Y.Wakamatsu и др., 1989. - 21 p. - Текст : непосредственный.

    Technical report / Nat. aerospace lab. TR-1440T : Effect of integration of scramjet into airframe on engine performance and payload / D.Akihisa,T.Kanda,K.Tani;D.Akihisa, T.Kanda, K.Tani et al., 2002. - 28 p. - Текст : непосредственный.

    Technical report / Nat. aerospace lab. TR-1442T : RJTF Mach 8 testing of a scramjet engine model of a contraction ratio of 8.3 with a strut / T.Kanda,K.Kudo,M.Izumikawa;T.Kanda, K.Kudo, M.Izumikawa et al., 2002. - 15 p. - Текст : непосредственный.

    Effect of sides-spillage from airframe on scramjet engine performance / K.Tani,T.Kanda,K.Kudo,D.Akihisa, 2000. - 21 p. - Текст : непосредственный.

    Experimental studies of supersonic film cooling with shock wave interaction / F.Ono,T.Kanda,M.Takahashi и др., 1995. - 13 p. - Текст : непосредственный.

    Technical report / Nat.aerospace lab. TR-1458 : Subscale wind tunnels and supplement studies of scramjet engine tests / T.Mitani,T.Hiraiwa,T.Kanda, 2003. - 232 p. - Текст : непосредственный.

    Kudo K. Preliminary study of thermal protection system of single-stage-to-orbit plane / K.Kudo,T.Kanda, 2000. - 10 p. - Текст : непосредственный.

    [Reports] / Amer.inst.of aeronautics and astronautics. N 89-2676 : comparison of scramjet engine performances among various cycles : Rep. presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf.,Monterey(Ca),July 10-12,1989 / T.Kanda,G.Masuya,Y.Wakamatsu и др, 1989. - 9 p. - Текст : непосредственный.

    [Reports] / Amer.inst.of aeronautics and astronautics. N 89-2680 : Mach 4 testing of scramjet inlet model : Rep. presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf.,Monterey(Ca),July 10-12,1989 / T.Kanda,T.Komuro,G.Masuya и др, 1989. - 8 p. - Текст : непосредственный.

    Effect of film cooling/regenerative cooling on scramjet engine performances / F.Ono,T.Kanda,G.Masuya и др., 1994. - 14 p. - Текст : непосредственный.

    Kanda T. Mach 4 testing of scramjet intel models. 1, 1991. - 54 p. - Текст : непосредственный.