Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 8 : Cooling Flow/heat Transfer Analysis User's Manual
- Heidegger, Nathan J.
- Sep 1, 1994.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Topp, David A., Hall, Edward J., and Delaney, Robert A.
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available. and Free-to-read Unrestricted online access
- The focus of this task was to validate the ADPAC code for heat transfer calculations. To accomplish this goal, the ADPAC code was modified to allow for a Cartesian coordinate system capability and to add boundary conditions to handle spanwise periodicity and transpiration boundaries. This user's manual describes how to use the ADPAC code as developed in Task 5, NAS3-25270, including the modifications made to date in Tasks 7 and 8, NAS3-25270.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19950005538., Accession ID: 95N11951., NASA-CR-195360., NAS 1.26:195360., and E-9025.
- No Copyright.
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