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Title   The effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests /
Format   online resource
Internet Access   https://purl.fdlp.gov/GPO/gpo143427  
Author   LinkWeick, Fred E., author.
Published   Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.
 
SuDoc Number   LinkY 3.N 21/5:6/322
Description   1 online resource (22 pages, 23 unnumbered pages) :  illustrations.
Content Type   text
Series   Link(Technical note (United States. National Advisory Committee for Aeronautics) ; 322.)
General Note   "October, 1929."
  No Federal Depository Library Program (FDLP) item number.
Bibliography   Includes bibliographical references (page 6).
Metadata Source   Description based on online resource, PDF version; title from title page (TRAIL, viewed August 19, 2020).
Subject - LC   LinkAirplanes -- Wings.
  LinkAirplanes -- Motors.
  LinkDrag (Aerodynamics)
  LinkWind tunnel testing.
Added Entry   LinkWood, Donald H., author.
Added Entry   LinkUnited States. National Advisory Committee for Aeronautics, issuing body.
Linking Field   LinkPrint version: Weick, Fred E. The Effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests (OCoLC)642700756
URL   Address at time of PURL creation  https://digital.library.unt.edu/ark:/67531/metadc54064/m2/1/high_res_d/19930081176.pdf  
 
Holdings   All items
 
OCLC Number   (OCoLC)1136490269
CGP Record Link   https://catalog.gpo.gov:443/F/?func=direct&doc_number=001128888&local_base=GPO01PUB
System Number   001128888


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