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Class 2 design update for the family of commuter airplanesThis is the final report of seven on the design of a family of commuter airplanes. This design effort was performed in fulfillment of NASA/USRA grant NGT-8001. Its contents are as follows: (1) the class 1 baseline designs for the commuter airplane family; (2) a study of takeoff weight penalties imposed on the commuter family due to implementing commonality objectives; (3) component structural designs common to the commuter family; (4) details of the acquisition and operating economics of the commuter family, i.e., savings due to production commonality and handling qualities commonality are determined; (5) discussion of the selection of an advanced turboprop propulsion system for the family of commuter airplanes, and (6) a proposed design for an SSSA controller design to achieve similar handling for all airplanes. Final class 2 commuter airplane designs are also presented.
Document ID
19880015245
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Creighton, Thomas R.
(Kansas Univ. Lawrence, KS, United States)
Hendrich, Louis J.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-182681
NAS 1.26:182681
Report Number: NASA-CR-182681
Report Number: NAS 1.26:182681
Accession Number
88N24629
Funding Number(s)
CONTRACT_GRANT: NGT-8001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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