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Concepts NREC COMPAL Ballot

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* 1. Please provide your contact information

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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. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 1	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 2	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 3	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 4	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 5	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 6	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 7	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 8	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 9	1. Create templates for application-specific compressor designs (e.g. turbocharger, refrigeration, turbo-expander) to minimize input for initial design estimate 10
2. Allow for creating user-specified design templates	2. Allow for creating user-specified design templates 1	2. Allow for creating user-specified design templates 2	2. Allow for creating user-specified design templates 3	2. Allow for creating user-specified design templates 4	2. Allow for creating user-specified design templates 5	2. Allow for creating user-specified design templates 6	2. Allow for creating user-specified design templates 7	2. Allow for creating user-specified design templates 8	2. Allow for creating user-specified design templates 9	2. Allow for creating user-specified design templates 10
3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 1	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 2	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 3	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 4	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 5	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 6	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 7	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 8	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 9	3. Allow specification of a stall point independent of the other models given a user defined minimum flow rate 10
4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project).	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 1	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 2	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 3	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 4	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 5	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 6	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 7	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 8	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 9	4. Implement a physics based design mode for return channels and continuous crossovers whereby the user inputs parameters such as diffusion ratio or pressure recovery along with exit swirl and the program calculates the geometry automatically (Note: multi-year project). 10
5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map)	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 1	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 2	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 3	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 4	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 5	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 6	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 7	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 8	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 9	5. Add capability to create a performance map with multiple variables simultaneously (e.g. multiple speed lines, IGV settings, efficiency on m-pr map) 10
6. Add ability to model IGVs and casing treatments simultaneously	6. Add ability to model IGVs and casing treatments simultaneously 1	6. Add ability to model IGVs and casing treatments simultaneously 2	6. Add ability to model IGVs and casing treatments simultaneously 3	6. Add ability to model IGVs and casing treatments simultaneously 4	6. Add ability to model IGVs and casing treatments simultaneously 5	6. Add ability to model IGVs and casing treatments simultaneously 6	6. Add ability to model IGVs and casing treatments simultaneously 7	6. Add ability to model IGVs and casing treatments simultaneously 8	6. Add ability to model IGVs and casing treatments simultaneously 9	6. Add ability to model IGVs and casing treatments simultaneously 10
7. Add ability to bleed and inject flow interstage on multi-stage machines	7. Add ability to bleed and inject flow interstage on multi-stage machines 1	7. Add ability to bleed and inject flow interstage on multi-stage machines 2	7. Add ability to bleed and inject flow interstage on multi-stage machines 3	7. Add ability to bleed and inject flow interstage on multi-stage machines 4	7. Add ability to bleed and inject flow interstage on multi-stage machines 5	7. Add ability to bleed and inject flow interstage on multi-stage machines 6	7. Add ability to bleed and inject flow interstage on multi-stage machines 7	7. Add ability to bleed and inject flow interstage on multi-stage machines 8	7. Add ability to bleed and inject flow interstage on multi-stage machines 9	7. Add ability to bleed and inject flow interstage on multi-stage machines 10
8. Add ability to create a preliminary design from an existing compressor map	8. Add ability to create a preliminary design from an existing compressor map 1	8. Add ability to create a preliminary design from an existing compressor map 2	8. Add ability to create a preliminary design from an existing compressor map 3	8. Add ability to create a preliminary design from an existing compressor map 4	8. Add ability to create a preliminary design from an existing compressor map 5	8. Add ability to create a preliminary design from an existing compressor map 6	8. Add ability to create a preliminary design from an existing compressor map 7	8. Add ability to create a preliminary design from an existing compressor map 8	8. Add ability to create a preliminary design from an existing compressor map 9	8. Add ability to create a preliminary design from an existing compressor map 10
9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 1	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 2	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 3	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 4	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 5	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 6	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 7	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 8	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 9	9. Allow for variable injection mass flow, (i.e. as a percentage of inlet mass flow) for performance map generation on multistage machines 10
10. Add ability to model vanes in casing treatment	10. Add ability to model vanes in casing treatment 1	10. Add ability to model vanes in casing treatment 2	10. Add ability to model vanes in casing treatment 3	10. Add ability to model vanes in casing treatment 4	10. Add ability to model vanes in casing treatment 5	10. Add ability to model vanes in casing treatment 6	10. Add ability to model vanes in casing treatment 7	10. Add ability to model vanes in casing treatment 8	10. Add ability to model vanes in casing treatment 9	10. Add ability to model vanes in casing treatment 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 for 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