Transonic Off Design Drag And Performance Of An Axisymmetric Inlet With 40 Percent Internal Contraction On Design
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Transonic Off Design Drag And Performance Of An Axisymmetric Inlet With 40 Percent Internal Contraction On Design
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Author : Richard R. Woollett
language : en
Publisher:
Release Date : 1974
Transonic Off Design Drag And Performance Of An Axisymmetric Inlet With 40 Percent Internal Contraction On Design written by Richard R. Woollett and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Transonic categories.
An experimental investigation determined the drag and pressure performance of an axisymmetric supersonic inlet when operated in the transonic speed range. The inlet configuration was derived from a Mach 2.5 mixed compression inlet design with assumed variable geometry. At typical engine airflows the drag coefficient varied from 0.057 to 0.192 when the Mach number changed from 0.80 to 1.27. The presence of a wing simulator resulted in a sizable increase in total drag at Mach 1.2. This interference drag, which is roughly a 0.1 increase in drag coefficient, originates equally from an increase in both additive and cowl pressure drag.
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1980
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aeronautics categories.
Transonic Off Design Drag And Performance Of An Axisymmetric Inlet With 40 Percent Internal Contraction On Design
DOWNLOAD
Author : Richard R. Woollett
language : en
Publisher:
Release Date : 1974
Transonic Off Design Drag And Performance Of An Axisymmetric Inlet With 40 Percent Internal Contraction On Design written by Richard R. Woollett and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Transonic categories.
An experimental investigation determined the drag and pressure performance of an axisymmetric supersonic inlet when operated in the transonic speed range. The inlet configuration was derived from a Mach 2.5 mixed compression inlet design with assumed variable geometry. At typical engine airflows the drag coefficient varied from 0.057 to 0.192 when the Mach number changed from 0.80 to 1.27. The presence of a wing simulator resulted in a sizable increase in total drag at Mach 1.2. This interference drag, which is roughly a 0.1 increase in drag coefficient, originates equally from an increase in both additive and cowl pressure drag.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1975
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Mechanics, Applied categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1974
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.
Monthly Catalog Of United States Government Publications
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Author :
language : en
Publisher:
Release Date : 1976
Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Government publications categories.
Monthly Catalog Of United States Government Publications Cumulative Index
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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1976
Monthly Catalog Of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with United States categories.
Bibliography On Aerodynamics Of Airframe Engine Integration Of High Speed Turbine Powered Aircraft
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Author : Mark R. Nichols
language : en
Publisher:
Release Date : 1980
Bibliography On Aerodynamics Of Airframe Engine Integration Of High Speed Turbine Powered Aircraft written by Mark R. Nichols and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aerodynamics categories.
Data Base For The Prediction Of Airframe Propulsion System Interference Effects
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Author :
language : en
Publisher:
Release Date : 1979
Data Base For The Prediction Of Airframe Propulsion System Interference Effects written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with categories.
Transonic Off Design Drag And Performance Of Three Mixed Compression Axisymmetric Inlets
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Author : Richard R. Woollett
language : en
Publisher:
Release Date : 1975
Transonic Off Design Drag And Performance Of Three Mixed Compression Axisymmetric Inlets written by Richard R. Woollett and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics, Transonic categories.