Evaluation of NACA0012 Airfoil Test Results in the NAL Two-Dimensional Transonic Wind Tunnel* | 東京工業大学附属図書館文献データベース

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Evaluation of NACA0012 Airfoil Test Results in the NAL Two-Dimensional Transonic Wind Tunnel*

著者名:

SUDANI, Norikazu

MATSUNO, Kenichi

TAKANASHI, Susumu

さらに 1 件

掲載資料名:

NASA Technical Reports

発行年:

1991

通号:

G6/02 0070484

ペーパー番号:

N92-21287

開始ページ:

1

終了ページ:

18

総ページ数:

18

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:

ZA00001428

類似資料:

1 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	7 テクニカルペーパー An Experimental Correlation Between Rotor Test and Wind Tunnel Ice Shapes on NACA 0012 Airfoils. Han, Y., Palacios, J.L. Society of Automotive Engineers
2 テクニカルペーパー New Dynamic Stability Equipment for Transonic Wind Tunnel Testing at NAL Ueno,Makoto, Miwa,Hitoshi American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Results of an Icing Test on a NACA 0012 Airfoil in the NASA Lewis Icing Research Tunnel Shin, Jaiwon, Bond, Thomas H. National Aeronautics and Space Adminstration
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 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	10 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
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 Numerical and Experimental Study of Drag Characteristics of HLFC Airfoils in High Subsonic, High Reynolds Number Flows Ishida,Yoji, Noguchi,Masayoshi, Sato,Mamoru, Kanda,Hiroshi Society of Automotive Engineering, Inc.
6 テクニカルペーパー TESTS ON 3 NACA 0012 AIRFOIL MODELS OF DFVLR IN THE NAL 0.3 TUNNEL: AN ASSESSMENT OF 2-D WALL INTERFERENCE Gopinath, R. et al. National Aeronautics and Space Administration	12 テクニカルペーパー THE SCHLIEREN OBSERVATION SYSTEM INSTALLED IN THE NAL TWO-DIMENSIONAL HIGH-REYNOLDS NUMBER TRANSONIC WIND TUNNEL AND ATTEMPTS TO IMPROVE IT Oguni, Yasuo et al. National Aeronautics and Space Administration

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