INIS
design
100%
allocations
100%
aviation fuels
100%
aircraft
100%
climates
100%
emission
50%
carbon dioxide
50%
cost
50%
optimization
41%
reduction
33%
profits
25%
hydrogen
25%
engines
25%
kerosene
25%
water vapor
16%
air quality
16%
fuels
16%
global warming
16%
range
16%
noise
16%
energy consumption
16%
increasing
8%
productivity
8%
operation
8%
network analysis
8%
levels
8%
ozone
8%
efficiency
8%
avoidance
8%
fuel consumption
8%
evaluation
8%
lifts
8%
speed
8%
altitude
8%
penalties
8%
soot
8%
mach number
8%
burns
8%
operating cost
8%
space
8%
sustainability
8%
liquids
8%
assessments
8%
drag
8%
solutions
8%
propulsion
8%
sulfates
8%
lifetime
8%
Engineering
Aircraft
100%
Design
100%
Aviation Fuels
100%
Temperature Response
88%
Reduction
44%
Optimization
33%
Powered Aircraft
33%
Research
33%
Fuel
33%
Evaluation
22%
Linear Temperature
22%
Models
22%
Engine
22%
Water
22%
Global Warming
22%
Air Quality
22%
Energy Engineering
22%
Multiobjective Optimization
11%
Design Objective
11%
Operating Cost
11%
Multiobjective Approach
11%
Propulsive Efficiency
11%
Turboprop Engines
11%
Electric Network Analysis
11%
Pressure Ratio
11%
Optimised Design
11%
Aviation
11%
Profitability
11%
Mach Number
11%
Noise Level
11%
Takeoff
11%
Objective Function
11%
Liquid Hydrogen
11%
Productivity
11%
Low Speed
11%
Design Optimization
11%
Airframe
11%
Low Altitude
11%
Lift to Drag Ratio
11%
Design Space
11%
Sustainable Development
11%
Keyphrases
Conceptual Evaluation
16%
Global Air Quality
16%
Turboprop Engine
16%
Hydrogen Aviation
16%