BOUNDARY LAYER PROFILE INVESTIGATIONS DOWNSTREAM OF AN AERO-ENGINE INTAKE ANTI-ICING AIR EXHAUST SLOT | 東京工業大学附属図書館文献データベース

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BOUNDARY LAYER PROFILE INVESTIGATIONS DOWNSTREAM OF AN AERO-ENGINE INTAKE ANTI-ICING AIR EXHAUST SLOT

著者名:: DOWNS, S. J. et al. ( ROLLS ROYCE LTD., DERBY, UK )
掲載資料名:: NASA Technical Reports(N88-)
発行年:: 1987
号:: PNR90378
ペーパー番号:: N88-11080
開始ページ:: 1
終了ページ:: 8
総ページ数:: 8
出版情報:: National Aeronautics and Space Administration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:

ZA00001424

類似資料:

1 テクニカルペーパー The influence of various exhaust geometrical parameters on the effectiveness of an aero-engine intake thermal anti-icing system Riley, S. J., James, E. H. The American Society of Mechanical Engineers	7 テクニカルペーパー A Multidisciplinary Aero-Engine Exhaust Emission Study. Shakariyants, S.A., Buijtenen, J.P., Visser, W.P.J., Tarasov, A. American Society of Mechanical Engineers
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5 テクニカルペーパー AN INVESTIGATION INTO ANTI-SWIRL DEVICES FOR S-SHAPED AIR INTAKES BACON, L. D., MAGOWAN, J. M. National Aeronautics and Space Administration	11 テクニカルペーパー Computational study of passive boundary layer control applied to a supersonic intake Watterson, J.K., Raghunathan, S. American Institute of Aeronautics and Astronautics
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