Skip to main navigation
Skip to search
Skip to main content
TU Delft Research Portal Home
Help & FAQ
Home
Research units
Researchers
Research output
Datasets
Projects
Press/Media
Prizes
Activities
Search by expertise, name or affiliation
Flight Mechanics and Performance of Direct Lift Control: Applying Control Allocation Methods to a Staggered Box-Wing Aircraft Configuration
C. Varriale
Flight Performance and Propulsion
Research output
:
Thesis
›
Dissertation (TU Delft)
193
Downloads (Pure)
Overview
Fingerprint
Research output
(4)
Fingerprint
Dive into the research topics of 'Flight Mechanics and Performance of Direct Lift Control: Applying Control Allocation Methods to a Staggered Box-Wing Aircraft Configuration'. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
INIS
control
100%
mechanics
100%
allocations
100%
lifts
100%
performance
100%
aircraft
100%
configuration
100%
surfaces
33%
aerodynamics
6%
design
3%
dynamics
3%
operation
3%
gravitation
3%
levels
3%
market
3%
motion
3%
pitch angle
3%
evaluation
3%
implementation
3%
comparative evaluations
3%
shape
3%
architecture
3%
drag
3%
Engineering
Wings
100%
Flight Mechanics
100%
Aircraft
80%
Obtains
20%
Deflection
20%
Decision Variable
10%
General Control
10%
Significant Change
10%
Aircraft Control
10%
Provide Suggestion
10%
Pitching Moment
10%
Flight Control
10%
Dynamic Behavior
10%
Problem Formulation
10%
Characteristics
10%
Aviation
10%
Transient Analysis
10%
Pitch Angle
10%
Aircraft Wing Model
10%
Design
10%