NACA0012 Airfoil Data Corrected for Sidewall Boundary-Layer Effects in the NAL Two-Dimensional Transonic Wind Tunnel

NACA0012 Airfoil Data Corrected for Sidewall Boundary-Layer Effects in the NAL Two-Dimensional Transonic Wind Tunnel

著者名:

SUDANI, Norikazu ( NATIONAL AEROSPACE LABLRATORY )

掲載資料名:

NASA Technical Reports

発行年:

1991

通号:

N92-28151

ペーパー番号:

N92-28151

開始ページ:

1

終了ページ:

75

総ページ数:

75

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 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	7 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
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 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.
3 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	9 テクニカルペーパー Cell structure on circular cylinders near the critical Reynolds number Yoshinaga, Takashi, Sato, Mamoru, Tate, Atsushi, Sudani, Norikazu, Soga, Kunio American Institute of Aeronautics and Astronautics
4 テクニカルペーパー R4 AIRFOIL DATA CORRECTED FOR SIDEWALL BOUNDARY-LAYER EFFECTS IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL Jenkins, R.V. National Aeronautics and Space Administration	10 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
5 テクニカルペーパー NASA SC(2)-0714 AIRFOIL DATE CORRECTED FOR SIDEWALL BOUNDARY-LAYER EFFECTS IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL Jenkins, Renaldo V. National Aeronautics and Space Administration	11 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
6 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	12 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

1

2

3

4

5

6

7

8

9

10

11

12