Turbine calculation force

bus line: No.126, about 3.9km

1. Walk about 20m from Panyu Square to Panyu Square Station

2. Take No.126, after 6 stops, to Panyu Central Hospital terminus (or take No.93)

3. Walk about 100m to Panyu central hospital

take the subway ring the day

Foreword
hypersonic vehicle technology
Chapter 1 Introction
1.1 hypersonic vehicle
1.2 research on the overall scheme of foreign hypersonic vehicles
1.2.1 reusable space vehicle
1.2.2 hypersonic aircraft
1.2.3 hypersonic cruise missile
1.3 development history of foreign hypersonic vehicle technology
1.3.1 brief history of hypersonic vehicle technology development abroad
1.3.2 development trend of hypersonic vehicle technology flight test abroad
1.3.3 other hypersonic vehicle technology development plans
1.4 main contents of this book
references
Chapter 2 Research on Key Technology Decomposition of hypersonic vehicle
2.1 Key Technology Decomposition of hypersonic vehicle
2.1.1 technical level and technical classification
2.1.2 Key Technology Decomposition Based on technology classification
2.2 the necessity of quantitative analysis in development strategy research
2.3 technical criticality analysis of hypersonic vehicle
2.4 hypersonic vehicle technology maturity analysis
2.4.1 technology maturity analysis model
2.4.2 application analysis of technology maturity in reusable space vehicles
2.5 hypersonic vehicle technology development path
references
Chapter 3 scramjet Technology
3.1 introction
3.2 concept and key technologies of supersonic combustion
3.2.1 proposal and concept of supersonic combustion
3.2.2 key technologies of supersonic combustion
3.3 component technology of scramjet
3.3.1 inlet
3.3.2 isolation section
3.3.3 combustion chamber
3.3.4 nozzle
3.4 overall performance evaluation index of scramjet
3.4.1 combustion efficiency
3.4.2 internal thrust
3.4.3 net thrust
3.4.4 thrust gain
3.4.5 selection of performance index
3.5 fuel technology of scramjet
3.6 ground test technology of scramjet
3.6.1 ground test system
3.6.2 direct connection test
3.6.3 free jet test
3.6.4 influence of test airflow parameters on engine performance
references
Chapter 4 hypersonic vehicle integrated propulsion system technology
4.1 rocket based combined cycle engine propulsion system
4.1.1 basic concept and working principle of RBCC
4.1.2 structure and principle of RBCC
4.1.3 influence factors of ejector rocket performance
4.1.4 research on RBCC engine performance analysis model
4.1.5 cycle scheme of RBCC system
4.2 turbo based combined cycle engine propulsion system
4.2.1 TBCC system scheme
4.2.2 mathematical model of TBCC turbine engine
4.2.3 TBCC intake and exhaust system
4.2.4 integration of TBCC propulsion system and hypersonic aircraft fuselage
4.3 other types of combined cycle engines
4.3.1 pre cooled turbine based combined cycle engine
4.3.2 deep cold vortex injection rocket combined cycle engine
4.3.3 LPG combined cycle engine
references
Chapter 5 hypersonic aircraft fuselage propulsion integrated design technology
5.1 hypersonic aerodynamics
5.1.1 hypersonic flow
5.1.2 calculation method of hypersonic aerodynamic engineering
5.1.3 numerical simulation technology of hypersonic flow
5.2 aerodynamic shape design of "waverider" for hypersonic vehicle
5.2.1 concept and aerodynamic characteristics of "waverider"
5.2.2 aerodynamic generation of waverider
5.2.3 design of waverider aircraft
5.3 integrated fuselage and propulsion design of hypersonic vehicle
5.3.1 hypersonic aircraft fuselage propulsion integrated force calculation system
5.3.2 integrated design of hypersonic vehicle forebody inlet
5.3.3 integrated design of hypersonic vehicle rear body nozzle
5.3.4 numerical calculation of aerodynamic propulsion integration for hypersonic vehicle
5.3.5 parametric modeling method for integrated geometry of hypersonic vehicle
5.4 integrated aerodynamic characteristics analysis of hypersonic vehicle
5.4.1 integrated aerodynamic characteristic calculation and modeling
5.4.2 influence of engine working state on integrated aerodynamic characteristics
5.4.3 influence of engine working state on aircraft stability and trim characteristics
5.4.4 influence of Afterbody nozzle design on integrated aerodynamic characteristics
5.5 integration of scramjet and waverider
5.5.1 main problems
5.5.2 aerodynamic shape design of waverider considering inlet conditions
5.5.3 design of "waverider" aerodynamic shape nozzle
5.6 integration of "circular section" propulsion system and hypersonic vehicle fuselage
5.6.1 "circle" of propulsion system? two-dimensional? The evolution of "circle"
5.6.2 integration of "circular section" propulsion system and hypersonic aircraft fuselage
references< Chapter 6 thermal protection technology of hypersonic vehicle
6.1 hypersonic vehicle thermal environment and thermal corridor
6.1.1 hypersonic vehicle thermal environment
6.1.2 hypersonic vehicle thermal corridor
6.1.3 engineering prediction method of hypersonic aerodynamic thermal environment
6.2 hypersonic aerodynamics? Hot? Basic research problems of elasticity
6.2.1 thermochemical reaction mechanism of high temperature reaction gas
6.2.2 hypersonic boundary layer transition
6.2.3 shock / shock interaction in hypersonic flow
6.2.4 aeroelasticity in hypersonic thermal environment
6.3 aerospace thermal protection technology and typical thermal protection system scheme
6.3.1 aerospace thermal protection technology
6.3.2 thermal protection system scheme of typical space shuttle
6.4 metal thermal protection system of reusable space vehicle
6.4.1 requirements for thermal protection system of reusable space vehicles
6.4.2 metal thermal protection system
6.4.3 thermal insulation materials for metal thermal protection system
6.4.4 thermal analysis method of metal thermal protection system
6.4.5 health monitoring technology of thermal protection system
6.5 thermal protection system and structural components of air breathing hypersonic vehicle
6.5.1 technical difficulties of thermal structure
6.5.2
6.5.3 control panel
references
Chapter 7 guidance and control technology of hypersonic vehicle
7.1 hypersonic vehicle navigation system technology
7.1.1 the role and significance of navigation system
7.1.2 integrated navigation technology
7.1.3 application of seeker and other task equipment in navigation system
7.2 hypersonic vehicle dynamics modeling technology
7.2.1 axisymmetric aircraft dynamics modeling
7.2.2 integrated dynamics modeling of hypersonic vehicle fuselage propulsion
7.2.3 hypersonic vehicle control modeling based on parametric shape
7.2.4 aerodynamic propulsion / aerodynamic coupling of hypersonic vehicles
7.3 hypersonic vehicle control and attitude measurement technology
7.3.1 control technology
7.3.2 embedded air data sensing system
7.4 guidance and control technology of hypersonic vehicle
7.4.1 main problems
7.4.2 flight control method
7.5 flight control technology of reusable space vehicle
7.5.1 characteristics of flight control system of reusable space vehicle
7.5.2 reusable flight control system design requirements
7.5.3 key technologies of reusable flight control system
references< Chapter 8 wind tunnel test techniques for hypersonic vehicles
8.1 tasks and requirements of hypersonic vehicle wind tunnel test
8.1.1 tasks of hypersonic vehicle wind tunnel test
8.1.2 requirements for hypersonic vehicle wind tunnel test
8.2 types of hypersonic wind tunnel equipment
8.2.1 overview of wind tunnel equipment
8.2.2 types of hypersonic wind tunnel equipment
8.3 hypersonic wind tunnel test form
8.3.1 full mold force test
8.3.2 pressure distribution measurement test
8.3.3 jet interference test
8.3.4 hypersonic inlet test
8.3.5 hinge moment test
8.3.6 interstage separation and multi-body separation test
8.4 hypersonic test wind tunnels abroad
8.4.1 overview of hypersonic wind tunnels abroad
8.4.2 lens series shock tunnel
8.4.3 ITAM hypersonic wind tunnel at? 303??
8.4.4 France S4 hypersonic wind tunnel
8.4.5 JAXA hypersonic wind tunnel
references
Part 2: hypersonic vehicle technology development in various countries
Chapter 9 US hypersonic vehicle technology research< br />9? The rise of scramjet (1950s)< br />9? 2. Early research on scramjet (1960s)< br />9? 3. Scram missile program (1961-1977)< br />9? 4 hypersonic research engine project (1964-1974)< br />9? 5. National aerospace program (1986-1995)< br />9? 5? 1. NASP proposal< br />9? 5? 2 NASP X? Conceptual design of 30 test aircraft< br />9? 5? 3. Research on key technologies in NASP program< br />9? 5? 4. Adjustment of NASP plan< br />9? 5? 5 the end of NASP program< br />9? 6 hypersonic technology program (1995-2003)< br />9? 6? 1 HyTech Program Overview< br />9? 6? The challenge of Technology< br />9? 6? 3. Main research achievements< br />9? 7 arrmd program (1998-2001)< br />9? 7? 1 battlefield demand for fast response missiles< br />9? 7? 2 design requirements and concept scheme< br />9? 7? 3. Technical challenges< br />9? 7? 4. Follow up development of arrmd program< br />9? 8 hyper? X plan and X? 43A flight test< br />9? 8? 1 hyper? X plan overview< br />9? 8? 2 X? Overall design of 43A test vehicle< br />9? 8? 3 X? 43A design and manufacturing challenge< br />9? 8? 4 X? 43A flight test< br />9? 9 NASA advanced space transportation hypersonic program< br />9? 9? 1 ASTP program< br />9? 9? 2. Technical approach< br />9? 9? 3 system analysis project< br />9? 9? 4. Promote technical projects< br />9? 9? 5 fuselage technology project< br />9? 9? 6 flight demonstration project< br />9? 10 HyFly program< br />9? 10? 1 concept / structure of aircraft< br />9? 10? 2 flight test process and test objectives< br />9? 10? 3 technical challenges< br />9? 11 X? 51A flight test program (2005 ~)< br />9? 11? 1. Strategic background< br />9? 11? 2. The origin of the plan< br />9? 11? 3 research team< br />9? 11? 4 planning path< br />9? 11? 5 test aircraft system composition< br />9? 11? 6 engine development and test< br />9? 11? 7 flight test plan arrangement< br />9? 11? 8 development of flight test< br />9? 12 Falcon plan< br />9? 12? 1 project background< br />9? 12? 2 turbine based combined cycle propulsion system< br />9? 12? 3 development of TBCC related technologies< br />9? 12? 4 HTV? 2 flight test
references
Chapter 10 technical research of Russian hypersonic vehicle< br />10? 1 "cold" plan< br />10? 1? 1 axisymmetric scramjet test model< br />10? 1? 2 flight test device< br />10? 1? 3 flight test< br />10? 2 "Eagle" project< br />10? 2? 1 Eagle test vehicle< br />10? 2? 2 scramjet test model< br />10? 2? 3 Eagle test vehicle< br />10? 2? 4 "Eagle" test< br />10? Rainbow? D2 plan< br />10? 3? Rainbow? D2 test aircraft< br />10? 3? 2 experimental scramjet model< br />10? 3? 3 flight test< br />10? 4 "eagle? "31" plan< br />10? 4? 1 flight test device< br />10? 4? 2 sub / scramjet test model< br />10? 4? 3 flight test< br />10? 5 hypersonic aircraft“