Aero Engineering - Thesis Research Subjects Wanted
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Join Date: Oct 2003
Location: Canberra Australia
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Aero Engineering - Thesis Research Subjects Wanted
An under graduate in Aeronatical Engineering and a wanabe Flight Test Engineer wants suggestions for his thesis subject.
My mini think tank produced the following.
Thresholds of acceleration sensitivities for the standard man/woman pilot.
Effects of experience limitations being imposed on current flight test personnel.
Factors for the setting of aircraft centre of gravity limits
Hazards of upper atmosphere cold soaked fuels for aircraft
Determination of optimum tensions in manual flight control cables.
Non destructive inspection (NDI) of load bearing composites in aircraft.
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Nominate your favourites in need of additional investigation/research.
My mini think tank produced the following.
Thresholds of acceleration sensitivities for the standard man/woman pilot.
Effects of experience limitations being imposed on current flight test personnel.
Factors for the setting of aircraft centre of gravity limits
Hazards of upper atmosphere cold soaked fuels for aircraft
Determination of optimum tensions in manual flight control cables.
Non destructive inspection (NDI) of load bearing composites in aircraft.
-------------
Nominate your favourites in need of additional investigation/research.
Thresholds of acceleration sensitivities for the standard man/woman pilot.
Effects of experience limitations being imposed on current flight test personnel.
Factors for the setting of aircraft centre of gravity limits
Hazards of upper atmosphere cold soaked fuels for aircraft
Determination of optimum tensions in manual flight control cables.
Non destructive inspection (NDI) of load bearing composites in aircraft.
There's an interesting list here, or here's a few ideas of mine.
- Take a commercial simulation (say on MS Flight Sim or X-plane) of something for which original flight test reports are available [the DC3 for example, many of the certification reports are available on the NASA document server] and conduct an evaluation of the integrity of the simulation.
- Find somebody friendly with a homebuilt aeroplane that has little documentation, and create a part 23/25 standard set of operating data for it. (Great one this, lots of flying, little risk, good technical rigour required).
- Invent and test an original method for measuring and standardising take-off and landing performance for light aeroplanes.
G
Well I'm not going to add any more topics, but I was rather curious at the page numbering in the link GTE gave: 'page 8 of 6'
Interesting subject though, and I look forward to seeing further suggestions.
Interesting subject though, and I look forward to seeing further suggestions.
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Thresholds of acceleration sensitivities for the standard man/woman pilot.
Good luck,
MrS
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Interaction of aerodynamic, hydrostatic and hydrodynamic forces in a seplane.
Seaplanes have a complex interaction of aerodynamic, hydrostatic and hydrodynamic forces during acceleration to take off speed.
A number of floatplanes are power limited and unable to transition from a low speed displacement taxi to high speed planing at high weights and/or high density altitudes.
The location of the center of gravity, the position of the elevators and flaps can determine whether the aircraft will accelerate through this high drag transition with the same load and wind. Different wind strengths and relative directions require different techniques.
These interactions could make for an intersting thesis.
A number of floatplanes are power limited and unable to transition from a low speed displacement taxi to high speed planing at high weights and/or high density altitudes.
The location of the center of gravity, the position of the elevators and flaps can determine whether the aircraft will accelerate through this high drag transition with the same load and wind. Different wind strengths and relative directions require different techniques.
These interactions could make for an intersting thesis.