Thesis
Hypersonic modelling and testing of space debris during planetary entry
- Abstract:
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In the study of atmospheric entry, some of the most challenging conditions to model numerically manifest in the slip and transition regimes. Denser than free molecular gases and sparser than continuum flows, these regimes are typically characterised by Knudsen numbers in the range 0.001 <= Kn <= 10. The complex interaction between gas particles in these sparse flows make the determination of aerothermal phenomena especially difficult, as traditional Navier-Stokes based CFD solutions ceas...
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Funding
+ Engineering and Physical Sciences Research Council
More from this funder
Programme:
National Wind Tunnel Facilities (NWTF)
Funding agency for:
Donaldson, N
Ireland, P
Funder identifier:
http://dx.doi.org/10.13039/501100000266
+ Science and Technology Facilities Council
More from this funder
Programme:
CASE studentship
Funding agency for:
Donaldson, N
Funder identifier:
http://dx.doi.org/10.13039/501100000271
Bibliographic Details
- Type of award:
- DPhil
- Level of award:
- Doctoral
- Awarding institution:
- University of Oxford
Item Description
- Language:
- English
- Keywords:
- Subjects:
- Deposit date:
- 2021-05-02
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