Flow Characteristics and Stability of Induced Shock Waves in the Isolator of Rotating Detonation Ramjet under Flight Mach Number 2.5 Conditions
AEROSPACE SCIENCE AND TECHNOLOGY(2023)
- Pretraining has recently greatly promoted the development of natural language processing (NLP)
- We show that M6 outperforms the baselines in multimodal downstream tasks, and the large M6 with 10 parameters can reach a better performance
- We propose a method called M6 that is able to process information of multiple modalities and perform both single-modal and cross-modal understanding and generation
- The model is scaled to large model with 10 billion parameters with sophisticated deployment, and the 10 -parameter M6-large is the largest pretrained model in Chinese
- Experimental results show that our proposed M6 outperforms the baseline in a number of downstream tasks concerning both single modality and multiple modalities We will continue the pretraining of extremely large models by increasing data to explore the limit of its performance

Low-Frequency Combustion Instability Mechanisms in A Side-Dump Combustor
被引用117
被引用55
Experimental Results of Shock Trains in Rectangular Ducts
被引用99
Effects of Dynamic Backpressure on Pseudoshock Oscillations in Scramjet Inlet-Isolator
被引用37
Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen
被引用65
Airbreathing Rotating Detonation Wave Engine Cycle Analysis
被引用181
被引用32
被引用51
Effects of Dynamic Backpressure on Shock Train Motions in Straight Isolator
被引用26
被引用66
Three-dimensional Modeling of Rotating Detonation in a Ramjet Engine
被引用161
Rotating detonation combustors and their similarities to rocket instabilities
被引用230
Effects of Flow-Field Structures on the Stability of Rotating Detonation Ramjet Engine
被引用31
Tip to End Analysis of Air Breathing Rotating Detonation Engine System
被引用1
Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines
被引用95
3D Problems of Rotating Detonation Wave in a Ramjet Engine Modeled on a Supercomputer.
被引用2
Hydrogen Fueled Detonation Ramjet: Conceptual Design and Test Fires at Mach 1.5 and 2.0
被引用19
被引用9
Pressure Feedback in the Diffuser of a Ram-RDE Propulsive Device
被引用12
被引用2
Air-breathing Rotating Detonation Fueled by Liquid Kerosene in Cavity-Based Annular Combustor
被引用44
Numerical Investigation of Contact Burning in an Air-Breathing Continuous Rotating Detonation Engine
被引用2
被引用12
Testing of Hydrogen-Fueled Detonation Ramjet in Aerodynamic Wind Tunnel at Mach 1.5 and 2.0
被引用1
被引用8
Reduction of Feedback Pressure Perturbation for Rotating Detonation Combustors
被引用5
被引用4