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Learjet model 25 drag analysisProcedures 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.
Document ID
19760003936
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ross, R.
(Gates Learjet Corp. Denver, CO, United States)
Neal, R. D.
(Gates Learjet Corp. Denver, CO, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Kansas Univ. Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N11024
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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