Technical Note

Technical Note
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Publisher :
Total Pages : 546
Release :
ISBN-10 : UIUC:30112008552892
ISBN-13 :
Rating : 4/5 (92 Downloads)

Synopsis Technical Note by :

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics
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Publisher :
Total Pages : 1274
Release :
ISBN-10 : RUTGERS:39030037544691
ISBN-13 :
Rating : 4/5 (91 Downloads)

Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Report

Report
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Publisher :
Total Pages : 40
Release :
ISBN-10 : STANFORD:36105024791886
ISBN-13 :
Rating : 4/5 (86 Downloads)

Synopsis Report by : United States. National Advisory Committee for Aeronautics

Index of NACA Technical Publications

Index of NACA Technical Publications
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Total Pages : 616
Release :
ISBN-10 : MSU:31293201271115
ISBN-13 :
Rating : 4/5 (15 Downloads)

Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics
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Publisher :
Total Pages : 996
Release :
ISBN-10 : CORNELL:31924089862860
ISBN-13 :
Rating : 4/5 (60 Downloads)

Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine

Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine
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Total Pages : 608
Release :
ISBN-10 : STANFORD:36105024796042
ISBN-13 :
Rating : 4/5 (42 Downloads)

Synopsis Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine by : Arthur M. Trout

Charts are presented by means of which the jet pressure ratio that give optimum division of power between propeller and jet for maximum total thrust power may be determined for any turbine-propeller engine with or without intercooling, reheat, regeneration, or any combination of these modifications.

NASA Technical Note

NASA Technical Note
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Total Pages : 412
Release :
ISBN-10 : MINN:31951000846241H
ISBN-13 :
Rating : 4/5 (1H Downloads)

Synopsis NASA Technical Note by :

Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics
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Publisher :
Total Pages : 988
Release :
ISBN-10 : UOM:39015006372802
ISBN-13 :
Rating : 4/5 (02 Downloads)

Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.