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ConceptsNREC AxCent Ballot

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* 2. Please apply a value to every item on the ballot (1-10, with 1 being no interest and 10 being critical).

	1	2	3	4	5	6	7	8	9	10
1. Add "tear drop" volute cross-section parameterization (for use in additive designs)	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 1	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 2	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 3	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 4	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 5	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 6	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 7	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 8	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 9	1. Add "tear drop" volute cross-section parameterization (for use in additive designs) 10
2. Allow AxCent to directly import parameterized AutoBlade geometries	2. Allow AxCent to directly import parameterized AutoBlade geometries 1	2. Allow AxCent to directly import parameterized AutoBlade geometries 2	2. Allow AxCent to directly import parameterized AutoBlade geometries 3	2. Allow AxCent to directly import parameterized AutoBlade geometries 4	2. Allow AxCent to directly import parameterized AutoBlade geometries 5	2. Allow AxCent to directly import parameterized AutoBlade geometries 6	2. Allow AxCent to directly import parameterized AutoBlade geometries 7	2. Allow AxCent to directly import parameterized AutoBlade geometries 8	2. Allow AxCent to directly import parameterized AutoBlade geometries 9	2. Allow AxCent to directly import parameterized AutoBlade geometries 10
3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project)	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 1	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 2	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 3	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 4	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 5	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 6	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 7	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 8	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 9	3. Create a layout tool that would include full rotating assembly including bearings and seals (Note: multi-year project) 10
4. Add parameterization for continuous cross-over pipe diffusers	4. Add parameterization for continuous cross-over pipe diffusers 1	4. Add parameterization for continuous cross-over pipe diffusers 2	4. Add parameterization for continuous cross-over pipe diffusers 3	4. Add parameterization for continuous cross-over pipe diffusers 4	4. Add parameterization for continuous cross-over pipe diffusers 5	4. Add parameterization for continuous cross-over pipe diffusers 6	4. Add parameterization for continuous cross-over pipe diffusers 7	4. Add parameterization for continuous cross-over pipe diffusers 8	4. Add parameterization for continuous cross-over pipe diffusers 9	4. Add parameterization for continuous cross-over pipe diffusers 10
5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 1	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 2	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 3	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 4	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 5	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 6	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 7	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 8	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 9	5. Add hub-to-shroud variable ("wedge angle") control for inducer sheared leading edges for use in blending that shear into the desired thickness distribution 10
6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive)	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 1	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 2	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 3	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 4	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 5	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 6	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 7	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 8	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 9	6. Add the ability to allow the user to select sign convention for blade angles (e.g. always positive) 10
7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 1	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 2	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 3	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 4	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 5	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 6	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 7	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 8	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 9	7. Allow for specifying the blade angle on the shroud at the exact point where the swept leading edge intersects the shroud 10
8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 1	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 2	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 3	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 4	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 5	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 6	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 7	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 8	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 9	8. Add parametric design of non-axisymmetric compressor inlet, or inlet plenum geometry, including non-axisymmetric IGVs 10
9. Add .txt file format export and import for camber chord and section parameters	9. Add .txt file format export and import for camber chord and section parameters 1	9. Add .txt file format export and import for camber chord and section parameters 2	9. Add .txt file format export and import for camber chord and section parameters 3	9. Add .txt file format export and import for camber chord and section parameters 4	9. Add .txt file format export and import for camber chord and section parameters 5	9. Add .txt file format export and import for camber chord and section parameters 6	9. Add .txt file format export and import for camber chord and section parameters 7	9. Add .txt file format export and import for camber chord and section parameters 8	9. Add .txt file format export and import for camber chord and section parameters 9	9. Add .txt file format export and import for camber chord and section parameters 10
10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius)	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 1	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 2	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 3	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 4	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 5	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 6	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 7	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 8	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 9	10. Add ability to design blade sections independent of spanwise position (i.e. at constant radius) 10
11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design)	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 1	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 2	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 3	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 4	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 5	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 6	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 7	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 8	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 9	11. Allow segment "swapping" between 2 *.des file (i.e. ability to swap a design in or out of a full stage design) 10
12. Allow multiple labyrinth seals in a single secondary flow path	12. Allow multiple labyrinth seals in a single secondary flow path 1	12. Allow multiple labyrinth seals in a single secondary flow path 2	12. Allow multiple labyrinth seals in a single secondary flow path 3	12. Allow multiple labyrinth seals in a single secondary flow path 4	12. Allow multiple labyrinth seals in a single secondary flow path 5	12. Allow multiple labyrinth seals in a single secondary flow path 6	12. Allow multiple labyrinth seals in a single secondary flow path 7	12. Allow multiple labyrinth seals in a single secondary flow path 8	12. Allow multiple labyrinth seals in a single secondary flow path 9	12. Allow multiple labyrinth seals in a single secondary flow path 10
13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 1	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 2	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 3	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 4	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 5	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 6	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 7	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 8	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 9	13. Allow independent splitter blade streamwise definition such that the trailing edge may be located inboard of the rotor OD 10
14. Create ability to define partial admission (including for drilled nozzles)	14. Create ability to define partial admission (including for drilled nozzles) 1	14. Create ability to define partial admission (including for drilled nozzles) 2	14. Create ability to define partial admission (including for drilled nozzles) 3	14. Create ability to define partial admission (including for drilled nozzles) 4	14. Create ability to define partial admission (including for drilled nozzles) 5	14. Create ability to define partial admission (including for drilled nozzles) 6	14. Create ability to define partial admission (including for drilled nozzles) 7	14. Create ability to define partial admission (including for drilled nozzles) 8	14. Create ability to define partial admission (including for drilled nozzles) 9	14. Create ability to define partial admission (including for drilled nozzles) 10
15. Add ability to have continuous blade from inducer through radial portion of a turbo pump	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 1	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 2	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 3	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 4	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 5	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 6	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 7	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 8	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 9	15. Add ability to have continuous blade from inducer through radial portion of a turbo pump 10

Please list up to two write-in items in the space below:

Question Title

* 3. Please rate the technical capability of this product:

1 Completely Unsatisfactory

2 Somewhat Useful But Needs Significant Improvement

3 Useful But Needs Improvement

4 Very Useful But Needs Minor Improvement

5 Completely Satisfactory

Or, put your own comments here:

Question Title

* 4. Please rate the technical support of this product:

1 Completely Unsatisfactory

2 Somewhat Useful But Needs Significant Improvement

3 Useful But Needs Improvement

4 Very Useful But Needs Minor Improvement

5 Completely Satisfactory

Or, put your own comments here:

Question Title

* 5. Would you recommend this product to a colleague?

Yes