Yoshio Wakamatsu

发表

Effect of Regenerative Cooling on Rocket Engine Specific Impulse

Goro Masuya, Takeshi Kanda, Masayuki Niino, 1994 .

Mach 8 testing of a scramjet engine with ramp compression

Noboru Sakuranaka, Takeshi Kanda, Atsuo Murakami, 2000 .

Experimental studies of supersonic film cooling with shock wave interaction

Toshihito Saito, Takeshi Kanda, Fumiei Ono, 1996 .

Design of Sub-Scale Rocket-Ramjet Combined Cycle Engine Model

Sadatake Tomioka, Shuuichi Ueda, Takeshi Kanda, 2005 .

Effects of injector geometry on scramjet combustor performance

Goro Masuya, Tomoyuki Komuro, Kenji Kudou, 1993 .

Mach 4 testing of scramjet inlet models

Goro Masuya, Tomoyuki Komuro, Takeshi Kanda, 1991 .

Some governing parameters of plasma torch igniter/flameholder in a scramjet combustor

Goro Masuya, Tomoyuki Komuro, Itsuro Kimura, 1993 .

Heating Evaluation Test of a Duct-shaped Cooling Structure Simulating Scramjet Combustors

Shuuichi Ueda, Toshihito Saito, Fumiei Ono, 2004 .

Effectiveness of plasma torches for ignition and flameholding in scramjet

Goro Masuya, Tomoyuki Komuro, Itsuro Kimura, 1989 .

Effect of film cooling/regenerative cooling on scramjet engine performances

Goro Masuya, Takeshi Kanda, G. Masuya, 1994 .