NASA NTRS · 19760003936
Learjet model 25 drag analysis
Abstract
Procedures and data for estimating drag were used to calculate the drag characteristics of the Model 25 airplane. Based on cruise flight test data obtained on the Model 25, these methods generally predicted the total drag characteristics within current acceptable and reasonable engineering accuracy.
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Ross, R., Neal, R. D.. 1975-01-01. Learjet model 25 drag analysis. https://ntrs.nasa.gov/citations/19760003936
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