Gledhill, Irvy MANordstrom, J2012-03-222012-03-222011-09Gledhill, 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 2011http://hdl.handle.net/10204/5667International Aerospace Symposium of South Africa, Pretoria, South Africa, 26-28 September 2011This 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.enArbitrary manoeuvreMomentumRocketsConference PresentationGledhill, I. M., & Nordstrom, J. (2011). Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames. http://hdl.handle.net/10204/5667Gledhill, Irvy MA, and J Nordstrom. "Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames." (2011): http://hdl.handle.net/10204/5667Gledhill IM, Nordstrom J, Characterisation of the flow regimes of arbitrary manoeuvre in absolute and relative frames; 2011. http://hdl.handle.net/10204/5667 .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 -