Design of the Circulation Control Wing STOL Demonstrator Aircraft
暂无分享,去创建一个
Robert J. Englar | Rodney A. Hemmerlyt | David W. Taylor | W. Horace Moore | J Vladimir Seredinsky | Walter Valckenaere | John A. Jackson | R. Englar | D. W. Taylor | W. Moore | J. V. Seredinsky | Walter Valckenaere | J. Jackson
[1] Robert J. Englar,et al. STOE Potential of the Circulation Control Wing for High-Performance Aircraft , 1978 .
[2] Robert J. Englar,et al. Subsonic Two-Dimensional Wind Tunnel Investigations of the High Lift Capability of Circulation Control Wing Sections , 1975 .
[3] Robert J. Englar,et al. Circulation Control -- An Updated Bibliography of DTNSRDC Research and Selected Outside References. , 1977 .
[4] Robert J. Englar,et al. Development of the A-6/Circulation Control Wing Flight Demonstrator Configuration , 1979 .
[5] Rodney A Hemmerly. An Investigation of the Performance of a J52-P-8A Engine Operating under the Influence of High Bleed Flow Extraction Rates. , 1977 .
[6] Robert L. Lopez Englar,et al. Circulation Control for High Lift and Drag Generation on STOL Aircraft , 1975 .
[7] John M Riebe. A Correlation of Two-dimensional Data on Lift Coefficient Available with Blowing-, Suction-, Slotted-, and Plain-flap High -lift Devices , 1955 .
[8] R. Englar,et al. Flight testing the circulation control wing , 1979 .