Journal of Propulsion Technology

2021 Vol.42	No.6	No.5	No.4	No.3	No.2	No.1
2020 Vol.41	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2019 Vol.40	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2018 Vol.39	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2017 Vol.38	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2016 Vol.37	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2015 Vol.36	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2014 Vol.35	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2013 Vol.34	No.12	No.11	No.10	No.9	No.8	No.7
	No.6	No.5	No.4	No.3	No.2	No.1
2012 Vol.33	No.6	No.5	No.4	No.3	No.2	No.1
2011 Vol.32	No.6	No.5	No.4	No.3	No.2	No.1
2010 Vol.31	No.6	No.5	No.4	No.3	No.2	No.1
2009 Vol.30	No.6	No.5	No.4	No.3	No.2	No.1
2008 Vol.29	No.6	No.5	No.4	No.3	No.2	No.1
2007 Vol.28	No.6	No.5	No.4	No.3	No.2	No.1
2006 Vol.27	No.6	No.5	No.4	No.3	No.2	No.1
2005 Vol.26	No.6	No.5	No.4	No.3	No.2	No.1
2004 Vol.25	No.6	No.5	No.4	No.3	No.2	No.1
2003 Vol.24	No.6	No.5	No.4	No.3	No.2	No.1
2002 Vol.23	No.6	No.5	No.4	No.3	No.2	No.1
2001 Vol.22	No.6	No.5	No.4	No.3	No.2	No.1
2000 Vol.21	No.6	No.5	No.4	No.3	No.2	No.1
1999 Vol.20	No.6	No.5	No.4	No.3	No.2	No.1
1998 Vol.19	No.6	No.5	No.4	No.3	No.2	No.1
1997 Vol.18	No.6	No.5	No.4	No.3	No.2	No.1
1996 Vol.17	No.6	No.5	No.4	No.3	No.2	No.1
1995 Vol.16	No.6	No.5	No.4	No.3	No.2	No.1
1994 Vol.15	No.6	No.5	No.4	No.3	No.2	No.1
1993 Vol.14	No.6	No.5	No.4	No.3	No.2	No.1
1992 Vol.13	No.6	No.5	No.4	No.3	No.2	No.1
1991 Vol.12	No.6	No.5	No.4	No.3	No.2	No.1
1990 Vol.11	No.6	No.5	No.4	No.3	No.2	No.1
1989 Vol.10	No.6	No.5	No.4	No.3	No.2	No.1
1988 Vol.9	No.6	No.5	No.4	No.3	No.2	No.1
1987 Vol.8	No.6	No.5	No.4	No.3	No.2	No.1
1986 Vol.7	No.6	No.5	No.4	No.3	No.2	No.1
1985 Vol.6	No.6	No.5	No.4	No.3	No.2	No.1
1984 Vol.5	No.4	No.3	No.2	No.1
1983 Vol.4	No.4	No.3	No.2	No.1
1982 Vol.3	No.4	No.3	No.2	No.1
1981 Vol.2	No.4	No.3	No.2	No.1
1980 Vol.1	No.2	No.1

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1 Computation of the integrated flow field around missile and mixed compression intake 9135

2 Experimental Investigation on Interaction Between Tip Clearance Flow and Three-Dimensional Separation in Compressor Cascade 8226

3 Calculating Performance of Pulse Detonation Turbo Engine 7110

4 Application and Analysis of γ-Reθ Transition Model in Hypersonic Flow 6920

5 Effect of Kerosene Distribution on Combustion Performance in Supersonic Combustor 6636

6 Application and development trend of electric propulsion technology 6565

7 Modeling of small perturbation state variable model for aeroengines 6551

8 Effects of nanometer PbCO 3 on combustion behavior of NEPE propellant 6123

9 Unsteady Numerical Investigation for Effects of Rim Sealing Flow on Performance of a Turbine Rotor 5990

10 Synthesis of nanometer-CuO powder and its effect on thermal decomposition characteristics of RDX 5924

1 Experimental Investigation on Interaction Between Tip Clearance Flow and Three-Dimensional Separation in Compressor Cascade 20949

2 Thrust Measurement of an Independent Microwave Thruster Propulsion Device with Three-Wire Torsion Pendulum Thrust Measurement System 15466

3 Unsteady Numerical Investigation for Effects of Rim Sealing Flow on Performance of a Turbine Rotor 6828

4 Application and development trend of electric propulsion technology 6334

5 Application and Analysis of γ-Reθ Transition Model in Hypersonic Flow 5934

6 A Study on Air Throttling Technology in Scramjet Combustor 5087

7 Effects of Blended Tip Winglet on Aerodynamic Performance of a Low Speed Compressor Rotor 4780

8 ExperimentalStudyonSparkIgnitionProcessofKerosenein 4469

9 Experimental Investigation on Detonation Devices Induce Detonation in Two-Phases Mixed Gas 3723

10 Study on NM/RDX/Nano-Al Pasty Propellant Property 3082

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