Aircraft Icing Research at NASA Glenn Research Center-Reference-Cited by-同舟云学术

Aircraft Icing Research at NASA Glenn Research Center

Published:2013-04 Issue:2 Volume:26 Page:260-276
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Potapczuk Mark G.¹

Affiliation:

1. Research Aerospace Engineer, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000322

Reference102 articles.

1. Acker L. W. (1948). “Preliminary results of natural icing of an axial-flow turbojet engine.” RM-E8C18 National Advisory Committee for Aeronautics Washington DC.

2. Addy H. E. Jr. (2000). “Ice accretions and icing effects for modern airfoils.” TP-2000-210031 NASA Washington DC.

3. Addy H. E. Jr. Miller D. R. and Ide R. F. (1997). “A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions.” TM-107424 NASA Cleveland.

4. Addy H. E. Jr. and Veres J. P. (2011). “An overview of NASA engine ice-crystal icing research.” TM-2011-217254 NASA Washington DC.

5. Anderson D. N. (2004). “Manual of scaling methods.” CR-2004-212875 NASA Washington DC.

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