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Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames

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dc.contributor.author Gledhill, Irvy MA
dc.contributor.author Nordstrom, J
dc.date.accessioned 2012-03-22T15:14:26Z
dc.date.available 2012-03-22T15:14:26Z
dc.date.issued 2011-09
dc.identifier.citation Gledhill, I and Nordstrom, J. Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames. International Aerospace Symposium of South Africa, Pretoria, South Africa, 26-28 September 2011 en_US
dc.identifier.uri http://hdl.handle.net/10204/5667
dc.description International Aerospace Symposium of South Africa, Pretoria, South Africa, 26-28 September 2011 en_US
dc.description.abstract This study concludes that: 1. the energy equation is expressed in terms of translations and rotational acceleration, 2. the generalised enthalpy equation is similarly expressed, 3. but the meaning of these is still to be explored, 4. dimensionless constants for momentum changes are re-derived, 5. but translational acceleration needs reconsideration in the light of numerical experiments, and rotational indications by Ro and Ek are that Taylor columns in rockets need consideration in terms of heat transfer, boundary conditions and compressibility. en_US
dc.language.iso en en_US
dc.relation.ispartofseries Workflow;8518
dc.subject Arbitrary manoeuvre en_US
dc.subject Momentum en_US
dc.subject Rockets en_US
dc.title Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames en_US
dc.type Conference Presentation en_US
dc.identifier.apacitation Gledhill, I. M., & Nordstrom, J. (2011). Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames. http://hdl.handle.net/10204/5667 en_ZA
dc.identifier.chicagocitation Gledhill, Irvy MA, and J Nordstrom. "Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames." (2011): http://hdl.handle.net/10204/5667 en_ZA
dc.identifier.vancouvercitation Gledhill IM, Nordstrom J, Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames; 2011. http://hdl.handle.net/10204/5667 . en_ZA
dc.identifier.ris TY - Conference Presentation AU - Gledhill, Irvy MA AU - Nordstrom, J AB - This study concludes that: 1. the energy equation is expressed in terms of translations and rotational acceleration, 2. the generalised enthalpy equation is similarly expressed, 3. but the meaning of these is still to be explored, 4. dimensionless constants for momentum changes are re-derived, 5. but translational acceleration needs reconsideration in the light of numerical experiments, and rotational indications by Ro and Ek are that Taylor columns in rockets need consideration in terms of heat transfer, boundary conditions and compressibility. DA - 2011-09 DB - ResearchSpace DP - CSIR KW - Arbitrary manoeuvre KW - Momentum KW - Rockets LK - https://researchspace.csir.co.za PY - 2011 T1 - Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames TI - Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames UR - http://hdl.handle.net/10204/5667 ER - en_ZA


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