Skip to main navigation
Skip to search
Skip to main content
The University of Brighton Home
Home
Profiles
Research units
Equipment
Projects
Research output
Activities
Student theses
Search by expertise, name or affiliation
Conceptual design of an aircraft for Mars mission
Agnieszka Kwiek
Advanced Engineering Centre
Research output
:
Contribution to journal
›
Article
›
peer-review
Overview
Fingerprint
Fingerprint
Dive into the research topics of 'Conceptual design of an aircraft for Mars mission'. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
Keyphrases
Mars Mission
100%
Mars
100%
Longitudinal Dynamic Stability
50%
Dynamic Stability Analysis
50%
Side Plate
50%
Tailless Aircraft
37%
Aircraft Configuration
37%
Tailless Configuration
25%
High-resolution
12%
Design Methodology
12%
Effective Method
12%
Damping Ratio
12%
Aerodynamics
12%
Aerodynamic Characteristics
12%
Bottom Plate
12%
Aerofoil
12%
Right Place
12%
Conceptual Design Phase
12%
Conceptual Study
12%
Plate Configuration
12%
MATLAB Code
12%
Period Characteristic
12%
Aircraft Aerodynamics
12%
Potential Flow Model
12%
Most Probable
12%
Engineering
Potential Flow
16%