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201. Payload to Low Earth Orbit by Aerospace Plane with Scramjet Engine

202. Design of Sub-scale Rocket-Ramjet Combined Cycle E

204. Concept Study of High-reliable LH2/LOX Rocket Engi

205. Nonpeptide orexin type-2 receptor agonist ameliorates narcolepsy-cataplexy symptoms in mouse models.

206. Pioglitazone lowers systemic asymmetric dimethylarginine by inducing dimethylarginine dimethylaminohydrolase in rats

207. Role of protein kinase C in Ca channel blocker-induced renal arteriolar dilation in spontaneously hypertensive rats--studies in the isolated perfused hydronephrotic kidney

208. Role of Rho-kinase and p27 in angiotensin II-induced vascular injury

209. Multidisciplinary Design Optimization of SSTO Space Plane Considering Rigid Body Characteristics

210. Momentum Balance Model of Flow Field with Pseudo-Shock

211. Aerodynamic Characteristics of the Combined Cycle Engine in an Ejector Jet Mode

212. Experimental Study of Downstream Combustion Ramjet-Mode

213. Auxiliary Injection for Combustion Augmentation of G/G Plume in a RBCC Combustor

214. Impulse function and drag in scramjet inlet models

215. Peroxisome Proliferator-Activated Receptor γ Ligands Inhibit Rho/Rho Kinase Pathway by Inducing Protein Tyrosine Phosphatase SHP-2

216. Scramjet Mode Tests of a Combined Cycle Engine Combustor

217. Scramjet Performance Achieved in Engine Tests from M4 to M8 Flight Conditions

219. Effect of Ingested Boundary Layer on Scramjet Engines' Thrust and Combustion Characteristics

220. Experimental Investigation of an Ejector-Jet

221. Measurement of mass capture ratio of scramjet inlet models

222. Two-Dimensional Range Search Based on the Voronoi Diagram

223. Suppression of Combustor- Inlet Interaction in a Scramjet Engine under M4 Flight Conditions

224. Effect of Airframe Configuration on Airflow Condition to Engine in Hypersonic Flow

225. Effect of Regenerative Cooling on Rocket Engine Specific Impulse

226. Altered renal microvascular response in Zucker obese rats

227. Distinct role of nitric oxide and endothelium-derived hyperpolarizing factor in renal microcirculation. Studies in the isolated perfused hydronephrotic kidney

228. Experiments on a Scramjet Engine with Ramp-Compression Inlet at Mach 8 Condition

229. A Conceptual Study of a Combined Cycle Engine for an Aerosapce Plane

231. Impact of calcium antagonists on bleeding time in patients with chronic renal failure

232. Modified water-cooled scramjet engine tested under M8 Condition

233. Dual-Mode Operation in a Scramjet Combustor

234. Effect of airframe geometry on thrust performance of aerospace plane

235. Mach 8 testing of a scramjet engine with ramp compression

237. Study of an airframe-integrated scramjet engine system

238. Effect of Airframe Integrated Configuration on Scramjet Inlet Performance

240. Propellant feed system of a regeneratively cooled scramjet

241. Mach 8 testing of scramjet engine models

242. Effects of Propellant Characteristics and Vehicle Structure on Rocket Space Plane

243. Development and application of ultra-high-temperature HIP by means of an optical temperature measurement system

244. Evaluation of Effectiveness of Periodic Flight by a Hypersonic Vehicle

245. Simulation of an airframe-integrated scramjet engine

246. Testing of a scramjet engine with a strut in M8 flight conditions

247. Study of the intensive combustion in the scramjet engine

248. Scramjet Inlet Flow Computations by Hybrid Grid Method

249. Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines.

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