Cover Image

GlennICE manual 4.2.0 /

Bibliographic Details
Main Author:	Porter, Christopher (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2024.
Series:	NASA technical memorandum ; 20240008077.
Subjects:	Fluid mechanics. Aerodynamics.
Online Access:	https://purl.fdlp.gov/GPO/gpo232379

Similar Items

Mixed phase modeling in GlennICE with application to engine icing /
by: Wright, William B., et al.
Published: (2011)

FUN3D manual : 13.7 /
by: Biedron, Robert T.
Published: (2020)

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
by: Penland, Jim A., et al.
Published: (1979)

A non-cut cell immersed boundary method for use in icing simulations /
by: Sarofeen, Christian M., et al.
Published: (2013)

Aero-thermal calibration of the NASA Glenn Icing Research Tunnel (2012 tests) /
by: Christine Pastor-Barsi, et al.
Published: (2013)

SmaggIce 2.0 : additional capabilities for interactive grid generation of iced airfoils /
Published: (2008)

Gas crossflow effects on airflow through a wire-form transpiration-cooling material /
by: Kaufman, Albert, 1928-, et al.
Published: (1972)

Design-of-experiments to reduce life-cycle costs in combat aircraft inlets /
by: Anderson, Bernhard H.
Published: (2003)

Design-of-experiments to reduce life-cycle costs in combat aircraft inlets /
by: Anderson, Bernhard H., et al.
Published: (2003)

Ice-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel /
by: Broeren, Andy P.
Published: (2016)

Lewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids /
by: Runyan, L. James
Published: (1992)

Aero-thermal calibration of the NASA Glenn Icing Research Tunnel (2004 and 2005 tests) /
Published: (2010)

Flow control applications /
by: Bushnell, Dennis M., et al.
Published: (2020)

Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of X-15A-2 airplane at Mach numbers from 1.75 to 4.63 /
by: Graves, Ernald B.
Published: (1969)

Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /
by: Broeren, Andy P.
Published: (2017)

Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel /
by: Broeren, Andy P., et al.
Published: (2012)

Modern airfoil ice accretions /
by: Addy, Harold E., Jr., 1960-, et al.
Published: (1997)

Manual for source flow characteristics program /
by: Kalben, Paul P.
Published: (1974)

High fidelity CFD analysis and validation of rotorcraft gearbox aerodynamics under operational and oil-out conditions : final report /
by: Kunz, Robert F.
Published: (2014)

Computer simulation of aircraft aerodynamics /
by: Inouye, Mamoru
Published: (1989)

Analysis of a hovering rotor in icing conditions /
by: Narducci, Robert
Published: (2012)

Icing encounter duration sensitivity study /
by: Addy, Harold E., Jr., 1960-
Published: (2011)

Unsteady aero computation of a 1 1/2 stage large scale rotating turbine /
by: To, Wai-Ming
Published: (2012)

Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove /
by: Bui, Trong T.
Published: (2014)

Preliminary aerodynamic investigation of fan rotor blade morphing /
by: Tweedt, Daniel L. (Daniel Lawrence)
Published: (2012)

Natural aerodynamics.
by: Scorer, R. S. (Richard Segar), 1919-
Published: (1958)

Characterization of the NASA Glenn Research Center 8-by 6-foot supersonic wind tunnel supersonic test section (2020 Test) /
by: Johnson, Aaron M., et al.
Published: (2020)

Swept-wing ice accretion characterization and aerodynamics /
by: Broeren, Andy P.
Published: (2013)

Prediction of turbulent diffusing flows using FUN3D /
by: Friedlander, David J., et al.
Published: (2022)

Aerodynamics of thrust vectoring by Navier-Stokes solutions /
by: Tseng, Jing-Biau, et al.
Published: (1991)

Rotary-wing relevant compressor aero research and technology development activities at Glenn Research Center /
Published: (2012)

Scaling of lift degradation due to anti-icing fluids based upon the aerodynamic acceptance test /
by: Broeren, Andy P., et al.
Published: (2012)

Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /
by: Batina, John T.
Published: (1985)

A user's guide to CGNS /
Published: (2001)

Analysis of inlet-compressor acoustic interactions using coupled CFD codes /
by: Suresh, A. (Writer on numeric analysis)
Published: (1998)

Variable-speed power-turbine research at Glenn Research Center /
Published: (2012)

Rime ice accretion and its effect on airfoil performance /
by: Bragg, Michael B., 1954-
Published: (1982)

Experimental investigation of shock-shock interactions over a 2D wedge at M=6 /
by: Mason, Michelle L.
Published: (2020)

An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 /
by: Prabhu, Ramadas K.
Published: (2001)

ASTROP2 users manual : a program for aeroelastic stability analysis of propfans /
by: Reddy, T. S. R., et al.
Published: (1996)