An Experimental Correlation Between Rotor Test and Wind Tunnel Ice Shapes on NACA 0012 Airfoils.

An Experimental Correlation Between Rotor Test and Wind Tunnel Ice Shapes on NACA 0012 Airfoils.

著者名:

掲載資料名:

2011 SAE International Conference on Aircraft & Engine Icing : technical paper

シリーズ名:

Society of Automotive Engineers technical paper series

シリーズ巻号:

2011

発行年:

2011

通号:

2011-38-0092

ペーパー番号:

2011-38-0092

総ページ数:

17

出版情報:

Warrendale, Penn.: Society of Automotive Engineers

ISSN:

01487191

言語:

英語

請求記号:

S10400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00052121
シリーズID:	PA00000058
会議名:	International Conference on Aircraft and Engine Icing and Ground Deicing
回次:	2011
会議開催地:	Chicago, IL, USA
会議開催年:	2011.06.13-2011.06.17
論文注記:	2011 International Conference on Aircraft and Engine Icing and Ground Deicing, June 13-17, 2011, Chicago, Illinois, USA

類似資料:

1 テクニカルペーパー A PIV Study of the Flow Around a NACA 0012 Airfoil in a Subsonic Wind Tunnel A. Avelar, L. dos Santos, O. de Faria Mello, J. Pagani American Institute of Aeronautics and Astronautics	7 テクニカルペーパー HIGH REYNOLDS NUMBER TRANSONIC TESTS ON A NACA 0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL Ladson, Charies L. et al. National Aeronautics and Space Administration
2 テクニカルペーパー Experimental and Computational Ice Shapes and Resulting Drag Increase for a NACA 0012 Airfoil Shin, Jaiwon, Bond, Thomas H. National Aeronautics and Space Adminstration	8 テクニカルペーパー AN EXPERIMENTAL MAPPING OF THE FLOW FIELD BEHIND A GLAZE ICE SHAPE ON A NACA 0012 AIRFOIL M.S. Thesis Final Report Spring, Samuel National Aeronautics and Space Administration
3 テクニカルペーパー A CRITICAL ASSESSMENT OF WIND TUNNEL RESULTS FOR THE NACA 0012 AIRFOIL McCroskey, W. J. National Aeronautics and Space Administration	9 テクニカルペーパー PRESSURE DISTRIBUTIONS FROM HIGH REYNOLDS NUMBER TRANSONIC TESTS OF AN NACA 0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL Ladson, Charies L. et al. National Aeronautics and Space Administration
4 テクニカルペーパー Evaluation of NACA0012 Airfoil Test Results in the NAL Two-Dimensional Transonic Wind Tunnel* SUDANI, Norikazu, KANDA, Hiroshi, SATO, Mamoru, MIWA, Hitoshi, MATSUNO, Kenichi, TAKANASHI, Susumu National Aeronautics and Space Adminstration	10 テクニカルペーパー NACA0012 Airfoil Data Corrected for Sidewall Boundary-Layer Effects in the NAL Two-Dimensional Transonic Wind Tunnel SUDANI, Norikazu, KANDA, Hiroshi, SATO, Mamoru, BABA, Shigeo, MIWA, Hitoshi, MATSUNO, Kenichi National Aeronautics and Space Adminstration
5 テクニカルペーパー Wall-Interference Assessment and Corrections for Transonic NACA 0012 Airfoil Data From Various Wind Tunnels Green, Lawrence L., Newman, Perry A. National Aeronautics and Space Adminstration	11 テクニカルペーパー An Experimental Study of the Aerodynamics of a NACA0012 Airfoil With a Simulated Glaze Ice Accretion-Volume II Bragg, Mike A. National Aeronautics and Space Adminstration
6 テクニカルペーパー PREDICTION OF ICE ACCRETION ON A SWEPT NACA 0012 AIRFOIL AND COMPARISONS TO FLIGHT TEST RESULTS Reehorst, Andrew L. National Aeronautics and Space Adminstration	12 テクニカルペーパー AN EXPERIMENTAL STUDY OF THE AERODYNAMICS OF A NACA 0012 AIRFOIL WITH A SIMULATED GLAZE ICE ACCRETION Interim Bragg, M.B. National Aeronautics and Space Administration

1

2

3

4

5

6

7

8

9

10

11

12