Ethanol Rocket: Difference between revisions

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=== Specific Heat ===
=== Specific Heat ===


The energy is transferred into pressure, sound, etc. The isochoric specific heat <math>C_v</math of air is <math>C_v = 0.7171</math> kJ/(kgK) at 18 centigrade. At 180 degrees Celsius <math>C_v = 0.7352</math> kJ/(kgK). Thus, the energy released heats
The energy is transferred into pressure, sound, etc. The isochoric specific heat <math>C_v</math> of air is <math>C_v = 0.7171</math> kJ/(kgK) at 18 centigrade. At 180 degrees Celsius <math>C_v = 0.7352</math> kJ/(kgK). Thus, the energy released heats


<math>  
<math>  
\begin{align}
\begin{align}
\Delta E &= C_v \Delta T m  \\
\Delta E &= C_v \Delta T m  \\
\Delta T &= \frac{\Delta E}{C_v m}
\Delta T &= \frac{\Delta E}{C_v m} \\
&=\frac{1.5 kJ}{0.7 kJ/(kgK) \times 0.5 \times 10^{-3}} \\
&=\frac{1.5 kJ}{0.7 kJ/(kgK) \times 0.5 \times 10^{-3}} \\
&= 2100 K
&= 2100 K
\end{align}
\end{align}
</math>
</math>


=== Ideal gas law ===
=== Ideal gas law ===

Revision as of 21:02, 31 May 2021

Introduction

Theory

Ethanol 3d model

Atom positions
-1.1712 0.2997 0.0000 O
-0.0463 -0.5665 0.0000 C
1.2175 0.2668 0.0000 C
-0.0958 -1.2120 0.8819 H
-0.0952 -1.1938 -0.8946 H
2.1050 -0.3720 -0.0177 H
1.2426 0.9307 -0.8704 H
1.2616 0.9052 0.8886 H
-1.1291 0.8364 0.8099 H

HCH bonds are assumed to be undistorded tetraherdal angle 109.5 degrees. Actually the electrons repeal each other. The HOC bond is 104.5 deg because. . .

Valence shell electron-pair repulsion theory (VSEPR theory). . .


Van der Waals radius
Atom Radius Relative radius
C 170 pm 1.42
H 120 pm 1.00
O 152 pm 1.27

Use CPK coloring convention, white (hydrogen), black (carbon) and red (oxygen).

Ethanol reaction with Oxygen and Air

Ethanol reaction with oxygen

The molecular weight of ethanol is g/mol, and the molar weight of oxygen is 32 g/mol. The oxygen--ethanol fuel ratio is . We need kg of oxygen to kg of ethanol. The air consists of 23.2 mass-% of oxygen, thus the air--ethanol ratio is .

The volume-% of oxygen in air is 20.9%. The volume of the bottle is ml which gives the amount of oxygen to be ml g of oxygen, which gives the amount of ethanol g ml. OR directly using air--ethanol ratio we have gram. That amount equals to ml mm3. Almost the same result using the methods. See the attached spreadsheet for detailed calculations.

The energy released by burning ethanol is 17.9 kJ/ml. Thus, ml of ethanol releases kJ of energy. This energy is converted into heat, sound and projectile motion (plus others).

Densities
Density At
Oxygen (g) 1.429 g/l STP
Oxygen (g) 1.314 g/l 20 °C
Ethanol (l) 789.45 g/l 20 °C
Air (l) 1.2041 g/l 20 °C

File:Ethanol oxygen combustion.ods

The inner diameter of the rocket bottle is 25 mm. The height of the ethanol in the cap need to be mm.

Exothermic Reaction and Energy release

Specific Heat

The energy is transferred into pressure, sound, etc. The isochoric specific heat of air is kJ/(kgK) at 18 centigrade. At 180 degrees Celsius kJ/(kgK). Thus, the energy released heats

Ideal gas law

The simplest idea is to use ideal gas law gives which gives force Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle F = pA} where </math>A</math> is the diameter of the nozzle.

Detonation velocity

Burn rate, detonation velocity. https://en.wikipedia.org/wiki/Table_of_explosive_detonation_velocities

http://www.explosionsolutions.co.uk/110411016.pdf

https://link.springer.com/article/10.1007/s00193-015-0554-7 Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle v=1500} m/s???


Horizontal(?) accelaration due to rapidly expanding air.

Benjamin Robins:

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle F(x) = \frac{RPAc}{x} }

where Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle x} distance in barrel, Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle R} is the initial ratio of hot gas pressure to atmospheric pressure, Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle P} is the atmospheric pressure, Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle A} is the cross-sectional area of the ball or bore, Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle c} is the length of the barrel occupied by the powder charge before ignition.

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle E_k = \int_0^L F(x) dx \iff v_0^2 = \frac{2RP}{m} \frac{\pi d^2 c}{4}\ln(L/c) }

where Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle d} is the barrel diameter (the bore)

The powder change Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle p} is given by Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle p= \frac{\pi d^2 c}{4}\eta } where Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \eta} is the density of gunpowder.


--

https://www.arc.id.au/RobinsOnBallistics.html

The pressure falls as Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle 1/x} .

--

Bernoulli?

--

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \sum F = 0 }


Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle F = ma = pA \iff F = m \frac{d^2x}{dt^2} }

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle F = m \frac{dv}{dt} = mv \frac{dv}{dx} = pA \iff mv dv = pA dx }

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \int mvdv = \int_0^L pA dx }

where

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \frac1L \int_0^L P dx = average pressure = \vec p }

If Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle A} is constant

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \frac12 mv^2 = A \int_0^L p dx = A \vec p L }

then

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle v = \sqrt{\frac{2\vec p A L}{m c_f}} } and Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \vec p = \frac{c_f mv^2}{2AL} }

Projectile friction, rotational energy, heat transfer: correction factor Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle c_f} .

The average pressure is 25% of peak pressure

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http://closefocusresearch.com/calculating-barrel-pressure-and-projectile-velocity-gun-systems

https://www.arc.id.au/CannonBallistics.html

Maximum Flying Distance

By the conservation of energy, all explosive energy is transferred into the kinetic energy.

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle E_\textrm{explosion}=E_\text{kinetic}}

The distance covered by a projectile with initial velocity $v_0$ is

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle s = \frac{v_0^2}{g}\sin(2\alpha) = \frac{}{}}

The drag coefficient Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle c_d} needs to be found. For the circular disc (a coin) the drag coefficient is almost constant for all velocities (Reynold numbers). The coefficient of drag for a cylinder in this orientation is about 0.81 so long as the length to diameter ratio is greater than 2, see http://www.aerospaceweb.org/question/aerodynamics/q0231.shtml. The cone in either end gives some complications.

The drag equation for the drag force is Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle F_D = \frac12 \rho v^2 c_d A} .

Piezo Crystal

To ignite the air--ethanol mixture, we use piezo crystal. When tjhe piezo crystal is compressed, it will generate an electric charge which creates a spark.

References

https://nptel.ac.in/content/storage2/courses/123106002/MODULE%20-%20I/Lecture%201.pdf

https://www.peacesoftware.de/einigewerte/o2_e.html

http://www.users.miamioh.edu/sommerad/NSF%20Files/drag_coefficient_calculation.pdf

DRAG COEFFICIENTS FOR FLAT PLATES , SPHERES, AND CYLINDERS MOVING AT LOW REYNOLDS NUMBERS IN A VISCOUS FLUID by ALVA MERLE JONES

http://www.aerospaceweb.org/question/aerodynamics/q0231.shtml

Ethanol rockets

https://www.youtube.com/watch?v=zTwz6FGobCA Ethanol Rocket - Cool Science Experiment


https://www.youtube.com/watch?v=4s-SZypWxeg Ethanol Explosion - Cool Science Experiment