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

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effect of Location of Aft-Mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-Wing Transport Airplane PDF full book. Access full book title Effect of Location of Aft-Mounted Nacelles on the Longitudinal Aerodynamic Characteristics of a High-Wing Transport Airplane by National Aeronautics and Space Adm Nasa. Download full books in PDF and EPUB format.

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

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...