A wind tunnel test of a tilt-body freewing aircraft including thrust effects

13th Applied Aerodynamics Conference

Volumn , Issue , 1995, Pages 1139-1149

  Chen, Weiping ^a   Barlow, Jewel B ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; ELEVATORS; WIND TUNNELS; WINGS;

AERODYNAMIC DATA; AERODYNAMIC FORCES; COMPLEX DESIGNS; COMPUTER SIMULATION MODEL; PROPELLER SLIPSTREAM; PROPULSION FORCE; UNIVERSITY OF MARYLAND; WIND TUNNEL TESTS;

FREEWING AIRCRAFT;

EID: 84963877271     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1995-1902     Document Type: Conference Paper

References (7)

1. Porter, R.F., Luce, R.G., Brown, J.H., “Evaluation of the Gust Alleviation Characteristics and Handling Qualities of a Free-wing Aircraft”, NASA CR-1523, July, 1970
2. Porter, R.F., Luce, R.G., Brown, J.H., “Investigation of the Application of the Free-Wing Principal to Light General Aviation Aircraft”, NASA CR-2046, June, 1972
3. Porter, R.F., et al “Analytical Study of the Free-Wmg Free- Trimmer Concept” NASA CR-2946, Feb., 1978
4. Weiping Chen & Jewe, L.B. Barlow “Stability, Control And Gust Response Characteristics of An Ultralight Freewing Airplane”, AIAA 924342, August,1992
5. Rae, William H. Jr., & Pope, Alan, Low Speed Wind Tunnel Testing, 2nd Ed., John Wiley & Sons, 1984
6. Weiping Chen & Jewel.B. Barlow “An ultralight Freewing Aircraft Design Study”, AIAA 924194, August, 1992
7. Weiping Chen, “GLenn. L. Martin Wind Tunnel Test Report on Freewing MK-11”, January 1990