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- {{AC|front=AC 3-08|description=Description_AC3-08|testdata=Test Case_AC3-08|cfdsimulations=CFD Simulations_AC3-08|evaluation=Evaluation_AC3 ...es of 5 mm. A description of the test case, the liquid properties, and the data is also available at:15 KB (2,258 words) - 16:08, 11 February 2017
- {{AC|front=AC 3-11|description=Description_AC3-11|testdata=Test Data_AC3-11|cfdsimulations=CFD Simulations_AC3-11|evaluation=Evaluation_AC3 ...o 6000, and the Grashof number (based on heat flux) ranges from 1.1x108 to 1.4x109. Such flows with strong buoyancy influences are found in a number of7 KB (1,126 words) - 16:14, 11 February 2017
- {{AC|front=AC 3-03|description=Description_AC3-03|testdata=Test Data_AC3-03|cfdsimulations=CFD Simulations_AC3-03|evaluation=Evaluation_AC3 =='''Comparison of Test data and CFD'''==5 KB (755 words) - 16:05, 11 February 2017
- {{AC|front=AC 2-07|description=Description_AC2-07|testdata=Test Case_AC2-07|cfdsimulations=CFD Simulations_AC2-07|evaluation=Evaluation_AC2 =='''Comparison of Test data and CFD'''==12 KB (1,533 words) - 15:35, 11 February 2017
- The goal of the study on which this AC is based has been to understand and control transfer applications [[Best_Practice_Advice_AC6-14#References|[1]]], or to reduce unwanted pressure pulsations6 KB (918 words) - 18:48, 11 February 2017
- {{AC|front=AC 4-03|description=Description_AC4-03|testdata=Test Data_AC4-03|cfdsimulations=CFD Simulations_AC4-03|evaluation=Evaluation_AC4 ...o model the temperature within the occupied zone (usually defined as up to 1.8m above floor level) given the value of the supply flow rate. Other import7 KB (1,094 words) - 16:41, 11 February 2017
- {{AC|front=AC 6-02|description=Description_AC6-02|testdata=Test Data_AC6-02|cfdsimulations=CFD Simulations_AC6-02|evaluation=Evaluation_AC6 ...case is provided by Hathaway et al. (1993, 1995). A considerable amount of data including static pressure profiles, total temperature and total pressure pr8 KB (1,204 words) - 16:53, 11 February 2017
- ...6-12 Quality Review|bestpractice=AC 6-12 Best Practice Advice|relatedUFRs=AC 6-12 Related ACs}} ...dering shock waves, reflected shock waves, wakes (compared to experimental data using pressure distribution or field of Mach number isolines). Behind of th16 KB (2,247 words) - 18:45, 11 February 2017
- {{AC|front=AC 2-06|description=Description_AC2-06|testdata=Test Data_AC2-06|cfdsimulations=CFD Simulations_AC2-06|evaluation=Evaluation_AC2 ...of the application challenge proposed by Partner 17, MTU Aero Engines. The AC is defined by the standard burner for confined natural gas flames that was7 KB (1,017 words) - 15:29, 11 February 2017
- ...iments carried out in a test rig at Volvo [[Best_Practice_Advice_AC2-12#1|[1,2,3]]]. Due to the simple geometry, this test case is quite attractive for verifying and validating new algorithms and mo6 KB (902 words) - 11:14, 16 August 2019
- {{AC|front=AC 3-01|description=Description_AC3-01|testdata=Test Data_AC3-01|cfdsimulations=CFD Simulations_AC3-01|evaluation=Evaluation_AC3 The topic chosen for study as the Application Challenge (AC) is that of 2-dimensional buoyancy-opposed plane wall jet penetrating into10 KB (1,461 words) - 15:47, 11 February 2017
- {{AC|front=AC 4-01|description=Description_AC4-01|testdata=Test Data_AC4-01|cfdsimulations=CFD Simulations_AC4-01|evaluation=Evaluation_AC4 ...Fluid Mechanics Ltd, on behalf of WS Atkins Consultants. A subset of this data is presented in this Application Challenge, namely the runway wind environm12 KB (1,971 words) - 16:35, 11 February 2017
- century, the studies providing quantitative data on this type of flow (see [[UFR_2-11_Description#table1|Table 1]]).13 KB (1,830 words) - 10:01, 7 September 2022
- {{AC|front=AC 3-02|description=Description_AC3-02|testdata=Test Data_AC3-02|cfdsimulations=CFD Simulations_AC3-02|evaluation=Evaluation_AC3 =='''Best Practice Advice for the AC'''==6 KB (983 words) - 16:02, 11 February 2017
- ...6-07 Quality Review|bestpractice=AC 6-07 Best Practice Advice|relatedUFRs=AC 6-07 Related ACs}} = Test Data =29 KB (4,256 words) - 12:52, 3 May 2018
- {{AC|front=AC 5-05|description=Description_AC5-05|testdata=Test Data_AC5-05|cfdsimulations=CFD Simulations_AC5-05|evaluation=Evaluation_AC5 ...ed data generated by Trombetti et al (1991), see [[#Measured data|Measured data]]. The free-stream velocity, U<sub>0</sub>, was 4m/s so that the Reynolds n12 KB (2,136 words) - 16:49, 11 February 2017
- {{AC|front=AC 6-02|description=Description_AC6-02|testdata=Test Data_AC6-02|cfdsimulations=CFD Simulations_AC6-02|evaluation=Evaluation_AC6 ...ens. Next, the air passes through a specially designed bellmouth with a 10:1 area contraction. From there it flows into the compressor and exits through16 KB (2,347 words) - 16:54, 11 February 2017
- {{AC|front=AC 5-05|description=Description_AC5-05|testdata=Test Data_AC5-05|cfdsimulations=CFD Simulations_AC5-05|evaluation=Evaluation_AC5 ...three hills and a corresponding set of three valleys (not covered in this AC document) were studied. A neutrally stable atmospheric boundary layer of he9 KB (1,384 words) - 16:48, 11 February 2017
- ...6-12 Quality Review|bestpractice=AC 6-12 Best Practice Advice|relatedUFRs=AC 6-12 Related ACs}} == Best Practice Advice for the AC ==13 KB (1,937 words) - 18:46, 11 February 2017
- {{AC|front=AC 1-05|description=Description_AC1-05|testdata=Test Data_AC1-05|cfdsimulations=CFD Simulations_AC1-05|evaluation=Evaluation_AC1 '''Application Challenge 1-05''' © copyright ERCOFTAC 200410 KB (1,593 words) - 10:36, 4 March 2024