A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings /

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Bibliographic Details
Main Author: Woodson, Shawn H.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors: DeJarnette, Fred R.
Format: Government Document Book
Language:English
Published: [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988.
Series:NASA contractor report ; NASA CR-4185.
Subjects:

MARC

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245 1 2 |a A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings /  |c Shawn H. Woodson and Fred R. DeJarnette. 
260 |a [Washington, DC] :  |b National Aeronautics and Space Administration, Scientific and Technical Information Division ;  |a [Springfield, Va.] :  |b [For sale by the National Technical Information Service],  |c 1988. 
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650 0 |a Boundary layer. 
650 0 |a Airplanes  |x Wings, Swept-back 
700 1 |a DeJarnette, Fred R. 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Division. 
740 0 |a Transonic interactive boundary layer theory for laminar and turbulent flow over swept wings. 
830 0 |a NASA contractor report ;  |v NASA CR-4185. 
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