Articles with tag: "analysis tools"

(Note: figures do not appear in the summaries below)
  1. Anti-Ice Heat Required Calculations with LEWICE

    Published: Mon 20 May 2024
    Updated: Tue 01 October 2024

    Aircraft A LEWICE ideice comparisons q
    Public domain image by Donald Cook.

    Prerequisites

    You need to have completed Anti-Ice Heat Required Calculations.

    Introduction

    Here, we will see that the values calculated by a multi-node analysis in LEWICE are comparable to the values calculated previously.

    Running LEWICE for anti-icing calculations involves (necessarily) more complex inputs. The user has to select which set of external heat transfer assumptions to use. The detailed output files require post-processing to extract the total heat required value.

    Discussion

    The LEWICE manual describes "deicer" cases that also may be used for anti-ice heat requirement analysis.
    An input is the "IDEICE" value in the case.inp file. By default, this is 0, and an unheated surface ice analysis is performed. However, with IDEICE > 0, ice protection analysis is performed, as detailed in a cased.inp file. A key input in that file is ievap, which for the cases below is set to ievap=1 …

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  2. Anti-Ice Heat Required Calculations

    Published: Mon 20 May 2024
    Updated: Tue 01 October 2024

    Aircraft A qr
    Public domain image by Donald Cook.

    Prerequisites

    You need to have completed Anti-Ice Heating Calculations Theory.

    Introduction

    For this we will use "Engineering Summary of Airframe Icing Technical Data", ADS-4, as the anti-ice examples are more detailed than those in the "Aircraft Icing Handbook", DOT/FAA/CT-88/8-1.

    The ADS-4 analysis method uses NACA-TN-2799, from 1952, for the heat and mass balance calculations. This method implements solutions as nomographs (for more details, see the post NACA-TN-2799). We will not be using the nomographs. The heat balance equations are similar to the Standard Computational Model, which we will use.

    The calculations are implemented in the file "aircraft_a_ads4.py" (and associated files) available at github.com/icinganalysis/icinganalysis.github.io. Readers are encouraged to run the analysis to the duplicate results.

    Discussion

    "Aircraft Icing", AC 20-73A, briefly mentions the terms Qa and Qr:

    Qa Heat available
    Qr Heat required

    Heat required is …

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  3. Anti-Ice Heating Calculations Theory

    Published: Mon 13 May 2024
    Updated: Tue 01 October 2024

    ADS-4 Figure 3-19. Typical external heat transfer coefficients for cylinder an flat plate.
    From ADS-4 apps.dtic.mil.

    Prerequisites

    You need to have completed Aircraft Icing Handbook Energy Balance Examples.

    Introduction

    We will review "Engineering Summary of Airframe Icing Technical Data", ADS-4 apps.dtic.mil, as the anti-ice examples are more detailed than those in the "Aircraft Icing Handbook", DOT/FAA/CT-88/8-1 apps.dtic.mil.

    We will also look at "Ice, Frost, and Rain Protection", SAE AIR1168/4 sae.org, for practical guidance for analysis.

    The ADS-4 and SAE AIR 1168/4 analysis methods use nomographs to implement graphical solutions. We will not be using the nomographs. While the notation is different, the analysis method from ADS-4 is very similar to the Standard Computational Model in the Aircraft Icing Handbook Merged Sections which we will use here.

    The energy balance equation is:

    Q"Source + Q"Sink = 0  
    

    Define Q"Sink by:
    Equation 2-50. Q"Sink = Q"conv + Q"DropWarm + Q"Evap

    Q"Sink = Q"conv + Q"DropWarm + Q"Evap  
    

    Define Q"Source …

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  4. Analysis Toolset

    Published: Mon 08 April 2024
    Updated: Tue 01 October 2024

    Figure 15 of NACA-TN-2904. Water-drop-trajectory analog.
Two investigators operate a large mechanical computer. 
One is seated turning a crank attached to a large cylinder labelled "Input Chart". 
The second operator turns another input chart crank. 
Another cylinder is labelled "Droplet Trajectories". 
There are many shafts and gears visible in the machine. 
Some machine parts are labelled with the differential equations of motion being solved.
    Figure 15 of NACA-TN-2904 ntrs.nasa.gov.

    Summary

    You will have to choose a toolset to perform the example analyses.

    Example calculations are provided in the Python programming language, and using the NASA-provided LEWICE code.

    Introduction

    You are highly encouraged to perform the analysis described in the examples (and not just read the examples). Some examples can be accomplished with hand calculations, while other require computational capabilities.

    You need to select your toolset.

    Consider your current and future uses

    A toolset is an investment of your time and resources. By performing the calculation of the examples used here, you will build your personal and software capabilities and skills.

    Your toolset at a particular time may not be entirely your choice. Your company, institution, or customer may have policies on which kinds of software are required, encouraged, discouraged, or prohibited. Some codes have by-country use restrictions. You may have signed an …

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