Study of Potential Aerodynamic Benefits From Spanwise Blowing at Wingtip | 東京工業大学附属図書館文献データベース

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Study of Potential Aerodynamic Benefits From Spanwise Blowing at Wingtip

著者名:: Raymond E. Mineck
掲載資料名:: NASA Technical Reports
発行年:: 1995
号:: NASA-TP-3515
パート:: NAS 1.60:3515
ペーパー番号:: N95-28669
開始ページ:: 1
終了ページ:: 102
総ページ数:: 102
出版情報:: National Aeronautics and Space Adminstration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:

ZA00001431

類似資料:

1 テクニカルペーパー ASSENSMENT OF POTENTIAL AERODYNAMIC BENEFITS FROM SPANWISE BLOWING AT THE WING TIP Mineck, Raymond Edward National Aeronautics and Space Adminstration	7 テクニカルペーパー WALL INTERFERENCE TESTS OF A CAST 10-2/DOA 2 AIRFOIL IN AN ADAPTIVE-WALL TEST SECTION Mineck, Raymond E. National Aeronautics and Space Administration
2 テクニカルペーパー Flow Visualization Studies of Blowing From the Tip of a Swept Wing Smith, Jannette W., Mineck, Raymond E., Neuhart, Dan H. National Aeronautics and Space Adminstration	8 テクニカルペーパー HARDWARE AND OPERATING FEATURES OF THE ADAPTIVE WALL TEST SECTION FOR THE 0.3-METER TRANSONIC CRYOGENIC TUNNEL Mineck, Raymond E. National Aeronautics and Space Administration
3 テクニカルペーパー Aerodynamic Characteristics and Pressure Distributions for an Executive-Jet Baselin Airfoil Section Allision, Dennis O., Mineck, Raymond E. National Aeronautics and Space Adminstration	9 テクニカルペーパー Wind-Tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings With Curvature of Quarter-Chord Line Mineck, Raymond E., Vijgen, Paul M.H.W. National Aeronautics and Space Adminstration
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5 テクニカルペーパー A Study of the Potential Benefits Associated with the Development of a Dedicated Helicopter Transmission Lubricant Drago,Raymond J., Mangione,Pasquale J., Wendrzycki,Raymond D. "Society of Automotive Engineering, Inc."	11 テクニカルペーパー Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section Dennis O. Allison, Raymond E. Mineck National Aeronautics and Space Adminstration
6 テクニカルペーパー Comparison of a Two-Demensional Adaprive-Wall Technique With Analytical Wall Interferece Correction Techniques Mineck, Raymond E. National Aeronautics and Space Adminstration	12 テクニカルペーパー Calibration of the 13- by 13-Inch Adaptive Wall Test Section for the Langley 0.3-Meter Transonic Cryogenic Tunnel Mineck, Raymond E., Hill, Acquilla S. National Aeronautics and Space Adminstration

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