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Download Application of a Performance Modeling Technique to an Airplane with Variable Sweep Wings by Paul C. Redin in PDF format completely FREE. No registration required, no payment needed. Get instant access to this valuable resource on PDFdrive.to!
About Application of a Performance Modeling Technique to an Airplane with Variable Sweep Wings
To calculate performance accurately for a specific airplane , the model must be adjusted and validated with actual flight test results. Reference 1
Detailed Information
| Author: | Paul C. Redin |
|---|---|
| Publication Year: | 2001 |
| Pages: | 33 |
| Language: | English |
| File Size: | 0.96 |
| Format: | |
| Price: | FREE |
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