In-flight aerodynamic measurements of an iced horizontal tailplane

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Ratvasky, Thomas P ^a   Van Zante, Judith Foss ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b Dynacs Engineering Company Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AEROSPACE ENGINEERING; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; DENSITY MEASUREMENT (OPTICAL); ELEVATORS; ICE; NASA; SOFTWARE TESTING; WIND STRESS; WIND TUNNELS;

AIRCRAFT DYNAMICS; FLIGHT AERODYNAMICS; FLIGHT CONDITIONS; PERFORMANCE LIMITS; QUASI-STEADY STATE; RANGE OF ANGLES OF ATTACK; RESEARCH PROGRAMS; WIND-TUNNEL TESTING;

AERODYNAMICS;

EID: 84982318883     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Ratvasky, T. P., “NASA/FAA Tailplane Icing Program Work Plan,” April 1994
2. Ingelman-Sundberg, M., Trunov, O.K., “Wind Tunnel Investigation Of The Hazardous Tail Stall Due To Icing,” Swedish-Soviet Working Group on Flight Safety Report No. JR-2. 1979
3. Trunov, O.K., Ingelman-Sundberg, M., “On The Problem Of Horizontal Tail Stall Due To Ice,” Swedish-Soviet Working Group on Flight Safety Report No. JR-3. 1985
4. Hiltner, D.W., McKee, M., La Noé, K.B., “DHC-6 Twin Otter Tailplane Airfoil Section Testing in The Ohio State University 7x10 Wind Tunnel,” 1995, being reviewed for publication
5. Gregorek, GM., Dreese, J.J., La Noé, K.B., “Additional Testing of the DHC-6 Twin Otter Iced Airfoil Section at The Ohio State University 7’xlO’ Wind Tunnel,” 1996, being reviewed for publication.