Effect of Location of Aft-Mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-Wing Transport Airplane PDF Download
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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...
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...
Author: National Aeronautics and Space Adm Nasa
Author: National Aeronautics and Space Adm Nasa
Author: William Kelly Abeyounis
Author: William Kelly Abeyounis
Author: William Kelly Abeyounis
Author: Lawrence Elwood Putnam
Author: Milton Lamb
Author: Lawrence Elwood Putnam
Author: 
Author: 
Author: Milton Lamb