| Issue |
Section |
Title |
File |
| Vol 10, No 2 (2016) |
Combustion, Explosion, and Shock Waves |
Thrust characteristics of an airbreathing pulse detonation engine in flight at mach numbers of 0.4 to 5.0 |
|
| Vol 10, No 2 (2016) |
Combustion, Explosion, and Shock Waves |
Thrust characteristics of a pulse detonation engine operating on a liquid hydrocarbon fuel |
|
| Vol 10, No 3 (2016) |
Combustion, Explosion, and Shock Waves |
Three-dimensional numerical simulation of the characteristics of a ramjet power plant with a continuous-detonation combustor in supersonic flight |
|
| Vol 10, No 3 (2016) |
Erratum |
Erratum to: “Three-dimensional numerical simulation of the operation process in a continuous detonation combustor with separate feeding of hydrogen and air” |
|
