Ice Formation

94 books
Documentation of ice shapes on the main rotor of a UH-1H helicopter in hoverJohn D. Lee

Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover

John D. Lee

1984No page data
Further investigations of icing effects on an advanced high-lift multi-element airfoilUnknown Author

Further investigations of icing effects on an advanced high-lift multi-element airfoil

Unknown Author

1995No page data
Validation results for LEWICE 2.0William B. Wright

Validation results for LEWICE 2.0

William B. Wright

1999No page data
Effects of ice accretion on aircraft aerodynamicsMichael B. Bragg

Effects of ice accretion on aircraft aerodynamics

Michael B. Bragg

1998No page data
Validation of NASA thermal ice protection computer codes.Unknown Author

Validation of NASA thermal ice protection computer codes.

Unknown Author

1996No page data
Collection efficiency and ice accretion calculations for a Boeing 737-300 inletColin S. Bidwell

Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet

Colin S. Bidwell

1997No page data
NASA's aircraft icing analysisRobert J. Shaw

NASA's aircraft icing analysis

Robert J. Shaw

1986No page data
Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wingUnknown Author

Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing

Unknown Author

1999No page data
Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wingUnknown Author

Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing

Unknown Author

1999No page data
Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wingUnknown Author

Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing

Unknown Author

1999No page data
The effects of the critical ice accretion on airfoil and wing performanceMichael S. Selig

The effects of the critical ice accretion on airfoil and wing performance

Michael S. Selig

1998No page data
Flight in adverse environmental conditionsNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 6h 17m

Flight in adverse environmental conditions

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1989377 pp.
Modern airfoil ice accretionsHarold E. Addy

Modern airfoil ice accretions

Harold E. Addy

1997No page data
Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests)E. Allen Arrington

Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests)

E. Allen Arrington

2000No page data
The measurement of aircraft performance and stability and control after flight through natural icing conditionsUnknown Author

The measurement of aircraft performance and stability and control after flight through natural icing conditions

Unknown Author

1986No page data
A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2Harold E. Addy

A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2

Harold E. Addy

1997No page data
Calculated performance of the NASA Lewis icing research tunnelLarry A. Viterna

Calculated performance of the NASA Lewis icing research tunnel

Larry A. Viterna

1991No page data
LWC and temperature effects on ice accretion formation on swept wings at glaze ice conditionsMario Vargas

LWC and temperature effects on ice accretion formation on swept wings at glaze ice conditions

Mario Vargas

2000No page data
Overview of the icing and flow quality improvements program for the NASA Glenn Icing Research TunnelUnknown Author

Overview of the icing and flow quality improvements program for the NASA Glenn Icing Research Tunnel

Unknown Author

2001No page data
Further evaluation of traditional icing scaling methodsDavid N. Anderson

Further evaluation of traditional icing scaling methods

David N. Anderson

1996No page data
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