| contributor author | J. A. Albers | |
| contributor author | N. O. Stockman | |
| date accessioned | 2017-05-08T22:58:36Z | |
| date available | 2017-05-08T22:58:36Z | |
| date copyright | January, 1975 | |
| date issued | 1975 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26714#1_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/87467 | |
| description abstract | The method and basic elements of computer solutions for both potential flow and viscous flow calculations for engine inlets are described. The procedure is applicable to subsonic conventional (CTOL), short-haul (STOL), and vertical takeoff (VTOL) aircraft engine nacelles operating in a compressible viscous flow. The calculated results compare well with measured surface pressure distributions for a number of model inlets. The paper discusses the uses of the program in both the design and analysis of engine inlets, with several examples given for VTOL lift fans, acoustic splitters, and for STOL engine nacelles. Several test support applications are also given. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Calculation Procedures for Potential and Viscous Flow Solutions for Engine Inlets | |
| type | Journal Paper | |
| journal volume | 97 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3445903 | |
| journal fristpage | 1 | |
| journal lastpage | 8 | |
| identifier eissn | 0742-4795 | |
| keywords | Engines | |
| keywords | Viscous flow | |
| keywords | Design | |
| keywords | Fans | |
| keywords | Computers | |
| keywords | Aircraft engines | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) AND Acoustics | |
| tree | Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 001 | |
| contenttype | Fulltext | |
