Effect of Location of Aft-mounted Nacelles on Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane PDF Download

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Effect of Location of Aft-mounted Nacelles on Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane

Effect of Location of Aft-mounted Nacelles on Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane PDF Author: William Kelly Abeyounis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 104

Book Description


Effect of Location of Aft-mounted Nacelles on Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane

Effect of Location of Aft-mounted Nacelles on Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane PDF Author: William Kelly Abeyounis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 104

Book Description


Effect of Under-wing Aft-mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane

Effect of Under-wing Aft-mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane PDF Author: William Kelly Abeyounis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 144

Book Description


Effect of Location of Aft-Mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-Wing Transport Airplane

Effect of Location of Aft-Mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-Wing Transport Airplane PDF Author: National Aeronautics and Space Adm Nasa
Publisher:
ISBN: 9781730995439
Category :
Languages : en
Pages : 102

Book Description
As part of a propulsion/airframe integration program at Langley Research Center, tests were conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of locating flow-through mixed flow engine nacelles in several aft underwing positions on the longitudinal aerodynamics of a high wing transport airplane. D-shaped inlet nacelles were used in the test. Some configurations with antishock bodies and with nacelle toe-in were also tested. Data were obtained for a free stream Mach number range of 0.70 to 0.85 and a model angle-of-attack range from -2.5 to 4.0 degrees. Abeyounis, William K. and Patterson, James C., Jr. Langley Research Center AERODYNAMIC INTERFERENCE; AIRCRAFT DESIGN; ENGINE AIRFRAME INTEGRATION; TRANSPORT AIRCRAFT; WING NACELLE CONFIGURATIONS; AFTERBODIES; FREE FLOW; MACH NUMBER; MULTIPHASE FLOW; PROPULSION SYSTEM CONFIGURATIONS; SYSTEMS INTEGRATION; TRANSONIC WIND TUNNELS...

Effect of Underwing Aft-mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane

Effect of Underwing Aft-mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-wing Transport Airplane PDF Author: William Kelly Abeyounis
Publisher:
ISBN:
Category :
Languages : en
Pages : 144

Book Description


Installation Effects of Wing-mounted Turbofan Nacelle-pylons on a 1/17 Scale, Twin-engine, Low-wing Transport Model

Installation Effects of Wing-mounted Turbofan Nacelle-pylons on a 1/17 Scale, Twin-engine, Low-wing Transport Model PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 112

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1786

Book Description


NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1224

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 486

Book Description