### Search result related to

Joule Thomson coefficient

**Notes**

**GEOTECHNICAL LABORATORY EXPERIMENTS**

**MG2351 PRINCIPLES OF MANAGEMENT**

**CE2028 GROUND WATER ENGINEERING**

**EE2151 CIRCUIT THEORY**

**CE 2041 BRIDGE STRUCTURES**

**CE 2034 INTRODUCTION TO SOIL DYNAMICS AND MACHINE FOUNDATION**

**GE2022 TOTAL QUALITY MANAGEMENT**

**CE2033 GROUND IMPROVEMENT TECHNIQUES**

**PH2111 Engineering Physics - I**

**PH2161 ENGINEERING PHYSICS II**

**Questions**

**One watt is equal to**

1 Answer

**One watt is equal to**

1 Answer

**Who discovered electron?**

2 Answer

**In a drainage area of 15 ha, the slope and drainage coefficient are 0.4% and 11 mm/day, respectively. The value of Manning’s roughness coefficient is 0.016. The inside diameter (in mm) of the corrugated plastic tubing used for drainage is**

0 Answer

**Consider an ideal vapor compression refrigeration cycle. If the throttling process is replaced by an isentropic expansion process, keeping all the other processes unchanged, which one of the following statements is true for the modified cycle?**

1 Answer

**Which one of the following can be considered as an appropriate pair of values of the regression coefficient of y on x and regression coefficient of x on y?**

0 Answer

**A set of tubs is pulled by a 15 tonne diesel locomotive at a gradient of 1 in 100 with an acceleration of 0.05 m/s2 . The coefficient of adhesion between the wheel and the track is 0.2 and the frictional resistance coefficient is 0.01. The maximum mass, in tonne, the locomotive can pull (rounded off to one decimal place) is _________.**

0 Answer

**Which of the following is not a basic unit in the S.I. System? (NIFT UG)**

1 Answer

**Mass transfer coefficient for equimolar counter-diffusion of water vapour in air is 0.4 m s^-1(based on concentration difference). Mass diffusivity of water vapour in air is 3 ×10-4 m^2s^-1. For 100 µm diameter droplet, the Sherwood Number (NSh) is**

1 Answer

**To compare biomass of a fish species in two lakes, A and B, a researcher records live- weights of 30 individuals from each lake. She assumes that these two datasets are normally distributed and have equal variance. She calculates Q= (x_A-x_B )/s where x_A and x_B are mean values from the respective lakes, and s is the pooled standard error. What is this quantity Q? (A) Correlation coefficient (B) Regression coefficient (C) t-statistic (D) χ2 -statistic**

0 Answer

**A horizontal axis drag type wind rotor, fitted with 4 thin rectangular blades having drag coefficient 1.29, is used to extract power when the average wind velocity in the rotor plane is 10 km h -1 . The maximum power coefficient is**

0 Answer

**Stream power is the product of specific weight of water with ________.**

0 Answer

**The maximum possible draft in cold rolling of sheet increases with the -gate-mechanical-2011**

1 Answer

**T he theoretical limit coefficient of variation (Vr in %) of the weight per unit length of cotton sliver is 𝑉𝑟 = 106/√𝑁, where N is the average number of fibres present in the crosssection of the sliver. To derive this expression, the coefficient of variation (in %) of the fibre weight per unit length, accurate to two decimal places, is considered as ______________**

0 Answer

**Segmental baffles in a 2-4 shell and tube heat exchanger (GATE-Chemical-Engg-2018)**

0 Answer

**Consider an airplane with a weight of 8000 N, wing area of 16 m2 , wing zero-lift drag coefficient of 0.02, Oswald’s efficiency factor of 0.8, and wing aspect ratio of 6, in steady level flight with wing lift coefficient of 0.375. Considering the same flight speed and ambient density, the ratio of the induced drag coefficient during steady level flight to that during a 30o climb is _______ (round off to 2 decimal places).**

0 Answer

**Semiconductor strain gages typically have much higher gage factors than those of metallic strain gages, primarily due to: GATE-Instrumentation-Engineering-2014**

1 Answer

**A thin airfoil is mounted in a low-speed, subsonic wind tunnel, in which the Mach number is 0.1. At a point on the airfoil, the pressure coefficient is measured to be 1.2. If the flow velocity is increased such that the free-stream Mach number is 0.6, the pressure coefficient at the same point on the airfoil will approximately be: (GATE-Aerospace-Engineering-2018)**

1 Answer

**For a steady laminar incompressible boundary layer flow over a sharp-edged flat plate at zero incidence,**

0 Answer

**The ideal static pressure coefficient of a diffuser with an area ratio of 2.0 is GATE-Aerospace Engineering-Question-2012**

1 Answer

**Speaks**

## You can do any of the following

Ask a question about thisWrite a not about this