dynamic systems analysis for turbine based aero propulsion systems

abstract: the aircraft engine design process seeks to optimize the overall system-level performance, weight, and cost for a given concept. steady-state simulations and data are used to identify trade-offs that should be balanced to optimize the

2016-09-08 09:24:50  

dynamic systems analysis for turbine based aero propulsion systems

abstract: the aircraft engine design process seeks to optimize the overall system-level performance, weight, and cost for a given concept. steady-state simulations and data are used to identify trade-offs that should be balanced to optimize the

2016-09-08 09:24:50  

dynamic systems analysis for turbine based aero propulsion systems

abstract: the aircraft engine design process seeks to optimize the overall system-level performance, weight, and cost for a given concept. steady-state simulations and data are used to identify trade-offs that should be balanced to optimize the

2016-09-08 09:24:50  

evolution of a planar wake in adverse pressure gradient

abstract: in the interest of improving the predictability of high-lift systems at maximum lift conditions, a series of fundamental experiments were conducted to study the effects of adverse pressure gradient on a wake flow. mean and fluctuating

2016-09-08 07:32:50  

evolution of a planar wake in adverse pressure gradient

abstract: in the interest of improving the predictability of high-lift systems at maximum lift conditions, a series of fundamental experiments were conducted to study the effects of adverse pressure gradient on a wake flow. mean and fluctuating

2016-09-08 07:32:50  

evolution of a planar wake in adverse pressure gradient

abstract: in the interest of improving the predictability of high-lift systems at maximum lift conditions, a series of fundamental experiments were conducted to study the effects of adverse pressure gradient on a wake flow. mean and fluctuating

2016-09-08 07:32:50  

initial evaluation of acoustic emission shm of prseus multi-bay box tests

abstract: a series of tests of the pultruded rod stitched efficient unitized structure (prseus) hwb multi-bay test article were conducted during the second quarter of 2015 at nasa langley research center (larc) in the combined loads test facilit

2016-08-29 10:54:53  

initial evaluation of acoustic emission shm of prseus multi-bay box tests

abstract: a series of tests of the pultruded rod stitched efficient unitized structure (prseus) hwb multi-bay test article were conducted during the second quarter of 2015 at nasa langley research center (larc) in the combined loads test facilit

2016-08-29 10:54:53  

initial evaluation of acoustic emission shm of prseus multi-bay box tests

abstract: a series of tests of the pultruded rod stitched efficient unitized structure (prseus) hwb multi-bay test article were conducted during the second quarter of 2015 at nasa langley research center (larc) in the combined loads test facilit

2016-08-29 10:54:53  

initial evaluation of acoustic emission shm of prseus multi-bay box tests

abstract: a series of tests of the pultruded rod stitched efficient unitized structure (prseus) hwb multi-bay test article were conducted during the second quarter of 2015 at nasa langley research center (larc) in the combined loads test facilit

2016-08-29 10:54:53  

initial evaluation of acoustic emission shm of prseus multi-bay box tests

abstract: a series of tests of the pultruded rod stitched efficient unitized structure (prseus) hwb multi-bay test article were conducted during the second quarter of 2015 at nasa langley research center (larc) in the combined loads test facilit

2016-08-29 10:54:53  

free-piston stirling power conversion unit for fission power system, phase ii final report

abstract: in phase ii, the manufacture and testing of two 6-kw(sub e)stirling engines was completed. the engines were delivered in an opposed 12-kw(sub e) arrangement with a common expansion space heater head. as described in the phase i report,

2016-08-29 07:11:53  

free-piston stirling power conversion unit for fission power system, phase ii final report

abstract: in phase ii, the manufacture and testing of two 6-kw(sub e)stirling engines was completed. the engines were delivered in an opposed 12-kw(sub e) arrangement with a common expansion space heater head. as described in the phase i report,

2016-08-29 07:11:53  

free-piston stirling power conversion unit for fission power system, phase ii final report

abstract: in phase ii, the manufacture and testing of two 6-kw(sub e)stirling engines was completed. the engines were delivered in an opposed 12-kw(sub e) arrangement with a common expansion space heater head. as described in the phase i report,

2016-08-29 07:11:53  

free-piston stirling power conversion unit for fission power system, phase ii final report

abstract: in phase ii, the manufacture and testing of two 6-kw(sub e)stirling engines was completed. the engines were delivered in an opposed 12-kw(sub e) arrangement with a common expansion space heater head. as described in the phase i report,

2016-08-29 07:11:53  

free-piston stirling power conversion unit for fission power system, phase ii final report

abstract: in phase ii, the manufacture and testing of two 6-kw(sub e)stirling engines was completed. the engines were delivered in an opposed 12-kw(sub e) arrangement with a common expansion space heater head. as described in the phase i report,

2016-08-29 07:11:53  

flat plate wake velocity statistics obtained with circular and elliptic trailing edges

abstract: the near wake of a flat plate with circular and elliptic trailing edges is investigated with data from direct numerical simulations. the plate length and thickness are the same in both cases. the separating boundary layers are turbulen

2016-08-29 06:27:53  

flat plate wake velocity statistics obtained with circular and elliptic trailing edges

abstract: the near wake of a flat plate with circular and elliptic trailing edges is investigated with data from direct numerical simulations. the plate length and thickness are the same in both cases. the separating boundary layers are turbulen

2016-08-29 06:27:53  

flat plate wake velocity statistics obtained with circular and elliptic trailing edges

abstract: the near wake of a flat plate with circular and elliptic trailing edges is investigated with data from direct numerical simulations. the plate length and thickness are the same in both cases. the separating boundary layers are turbulen

2016-08-29 06:27:53  

flat plate wake velocity statistics obtained with circular and elliptic trailing edges

abstract: the near wake of a flat plate with circular and elliptic trailing edges is investigated with data from direct numerical simulations. the plate length and thickness are the same in both cases. the separating boundary layers are turbulen

2016-08-29 06:27:53  

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