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Title   Analysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning /
Format   online resource
Internet Access   https://purl.fdlp.gov/GPO/gpo141403  
Author   LinkFeder, Melvin S., author.
Published   Washington, [D.C.] : National Advisory Committee for Aeronautics, 1950.
 
SuDoc Number   LinkY 3.N 21/5:6/2183
Description   1 online resource (39 pages) :  illustrations.
Content Type   text
Series   Link(Technical note (United States. National Advisory Committee for Aeronautics) ; 2183.)
General Note   "September 1950."
  No Federal Depository Library Program (FDLP) item number.
Bibliography   Includes bibliographical references (page 35).
Metadata Source   Description based on online resource, PDF version; title from title page (TRAIL, viewed July 15, 2020).
Subject - LC   LinkAirplanes -- Control systems.
  LinkAirplanes -- Turbine-propeller engines.
  LinkAirplanes -- Turbofan engines -- Afterburners.
  LinkMathematical analysis.
  LinkTransfer functions.
Added Entry   LinkHood, Richard, author.
Added Entry   LinkUnited States. National Advisory Committee for Aeronautics, issuing body.
Linking Field   LinkPrint version: Feder, Melvin S., Analysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning (OCoLC)663904378
URL   Address at time of PURL creation  https://digital.library.unt.edu/ark:/67531/metadc55777/m2/1/high_res_d/19930083125.pdf  
 
Holdings   All items
 
OCLC Number   (OCoLC)1104148323
CGP Record Link   https://catalog.gpo.gov:443/F/?func=direct&doc_number=001126258&local_base=GPO01PUB
System Number   001126258


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