Fabignon et al., 2016 - Google Patents
Recent advances in research on solid rocket propulsionFabignon et al., 2016
View PDF- Document ID
- 12577935701197132061
- Author
- Fabignon Y
- Anthoine J
- Davidenko D
- Devillers R
- Dupays J
- Gueyffier D
- Hijlkema J
- Lupoglazoff N
- Lamet J
- Tessé L
- Guy A
- Erades C
- Publication year
- Publication venue
- Aerospace Lab
External Links
Snippet
This paper is devoted to a review of some recent studies conducted at ONERA within the framework of solid rocket propulsion for missiles, as well as space launchers. The viewpoint adopted is to present the physical phenomena studied using modeling, simulations and …
- 239000007787 solid 0 title abstract description 59
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Fabignon et al. | Recent advances in research on solid rocket propulsion | |
| Wright et al. | Data-parallel line relaxation method for the Navier-Stokes equations | |
| Simmons | Rocket exhaust plume phenomenology | |
| Hertzberg et al. | Ram accelerator-A new chemical method for accelerating projectilesto ultrahigh velocities | |
| Kailasanath | Review of propulsion applications of detonation waves | |
| MacLean et al. | Numerical and experimental characterization of high enthalpy flow in an expansion tunnel facility | |
| Scherrer et al. | Recent CEDRE applications | |
| Martinez Schramm et al. | Ground testing of the HyShot II scramjet configuration in HEG | |
| Niu et al. | A simplified model for fast estimating infrared thermal radiation of low-altitude under-expanded exhaust plumes | |
| Doisneau | Eulerian modeling and simulation of polydisperse moderately dense coalescing spray flows with nanometric-to-inertial droplets: application to Solid Rocket Motors | |
| Edquist et al. | Comparison of Navier-Stokes flow solvers to Falcon 9 supersonic retropropulsion flight data | |
| Bonelli et al. | Preliminary design of a hypersonic air-breathing vehicle | |
| Stowe et al. | Effect of flight and motor operating conditions on infrared signature predictions of rocket exhaust plumes | |
| Nelson | Radiative heating in scramjet combustors | |
| Rana et al. | Dynamics of sonic hydrogen jet injection and mixing inside scramjet combustor | |
| Leibowitz et al. | Hypervelocity spherically-blunted cone flows in Mars entry ground testing | |
| Panchal et al. | In Silico Design of Detonation-Free High-Performance Dual-Thrust Solid and Hybrid Propellant Rockets Through the Application of the Chapman–Jouguet Condition | |
| de Paula Toro | Aerothermodynamic design, manufacturing and testing of a 3-d prototyped scramjet | |
| Steelant et al. | Comparison of supersonic combustion tests with shock tunnels, flight and CFD | |
| Son et al. | Refined mode classification and performance analysis method of dual-mode scramjet vehicles for flight trajectory optimization | |
| Viviani et al. | Effect of finite rate chemical models on the aerothermodynamics of reentry capsules | |
| Hoste | Scramjet combustion modeling using eddy dissipation model | |
| Brandyberry et al. | Rocstar simulation suite: An advanced 3-D multiphysics, multiscale computational framework for tightly coupled, fluid-structure-thermal applications | |
| Drummond | Development of methods to predict high-speed reacting flows in aerospace propulsion systems | |
| Corbin | Design and analysis of a Mach 3 dual mode scramjet combustor |