In-flight aerodynamic measurements of an iced horizontal tailplane-Reference-Cited by-同舟云学术

In-flight aerodynamic measurements of an iced horizontal tailplane

Published:1999-01-11 Issue: Volume: Page:
ISSN:
Container-title:37th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Ratvasky Thomas¹,Van Zante Judith²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Dynacs Engineering Co., Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-638

Reference14 articles.

1. 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

2. 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 No& K.B. "DHC-6

3. Twin Otter Tailplane Airfoil Section Testing in The Ohio StateUniversity 7x10 Wind Tunnel," 1995, being reviewed for publication 5 Gregorek, GM., Dreese,J.J.,La No& K.B.

4. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188

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