Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel

被引：0
|
作者：
Jenkins, Renaldo V. [1 ]
Hill, Acquilla S. [1 ]
Ray, Edward J. [1 ]
机构：
[1] NASA Langley Research Cent, United States
来源：
NASA Technical Memorandum | 1988年 / 4044期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 6 条
  • [1] HIGH REYNOLDS NUMBER TESTS OF THE NASA SC(2)-0012 AIRFOIL IN THE LANGLEY 0. 3-METER TRANSONIC CRYOGENIC TUNNEL.
    Mineck, Raymond E.
    Lawing, Pierce L.
    NASA Technical Memorandum, 1987,
  • [2] Application of Resonant Femtosecond Tagging Velocimetry in the 0.3-Meter Transonic Cryogenic Tunnel
    Reese, Daniel
    Danehy, Paul
    Jiang, Naibo
    Felver, Josef
    Richardson, Daniel
    Gord, James
    AIAA JOURNAL, 2019, 57 (09) : 3851 - 3858
  • [3] Application of resonant femtosecond tagging velocimetry in the 0.3-meter transonic cryogenic tunnel
    Reese, Daniel
    Danehy, Paul
    Jiang, Naibo
    Felver, Josef
    Richardson, Daniel
    Gord, James
    AIAA Journal, 2019, 57 (09): : 3851 - 3858
  • [4] PRESSURE DISTRIBUTIONS FROM HIGH REYNOLDS NUMBER TESTS OF A BOEING BAC I AIRFOIL IN THE LANGLEY 0. 3-METER TRANSONIC CRYOGENIC TUNNEL.
    Johnson Jr., William G.
    Hill, Acquilla S.
    NASA Technical Memorandum, 1985,
  • [5] Characterization of naturally-occurring particles in the NASA Langley 0.3-m Transonic Cryogenic Tunnel using PTV
    Burns, Ross A.
    Gao, Jian
    Danehy, Paul M.
    AIAA SCITECH 2024 FORUM, 2024,
  • [6] CFD STUDY OF EFFECTS OF BOUNDARY LAYER SUCTION ON TRANSONIC SC(2)-0714 AIRFOIL PERFORMANCE
    Khamedov, Ruslan
    Baitlessov, Ruslan
    Rojas-Solorzano, Luis
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2017, VOL 7, 2018,
1