Quantcast
  
Home
From the Magazines
Online Exclusives
Event Calendar
Event Coverage
Product News
Hot News
On the Flightline
Article Archives
Videos
The Radio Control Show
Plans Guide
In the Hangar
Builders' Bash
Upload your Plane
Blogs
Forums
Related Links
Site Search
Customer Service
Contact Us




Nitromethane Bonus Material

 
(6/18/2009)

By Dave Gierke

The Dooling Brothers reported a 1,500rpm increase in shaft speed when using Arden’s Formula B compared with the standard mix of methanol and castor oil. The engine, a .61ci-displacement, single cylinder unit, produced 1.5 bhp at 15,600rpm on the methanol/castor oil fuel; since the engine speeded-up to 17,100rpm with the same propeller, we can determine the new power output by using Power Factor calculations:

Bhp2 = bhp1 (rpm2 ÷ rpm1)3

Bhp2 = 1.5 (17,100 ÷ 15,600)3

Bhp2 = 1.5 (1.096)3

Bhp2 = 1.5 (1.32)

Bhp2 = 1.98 … a 32% boost in power. (Bhp2 - bhp1 bhp1 = (1.98 - 1.5) ÷1.5 = 0.32

 

SPECIFIC ENERGY

Internal combustion engine enthusiasts often struggle to understand why fuels such as nitromethane produce more power than other fuels, such as gasoline, which has almost four times more heating value (19,000 btu/lb. vs. 4,850 btu/lb.). The question is best approached from the perspective of specific energy (SE). A fuel’s specific energy is calculated by dividing its heating value by its air/fuel ratio (btu/lb. ÷ A/F). The result represents the fuel’s heat energy delivered per pound of air inducted into the engine. To demonstrate the value of specific energy calculations, notice that nitromethane has 217% more SE than gasoline at their peak-power air/fuel ratios (4850 - 1532) ÷ 1532 = 2.17. In Chart A, nitromethane is compared to both gasoline and methanol.

 

Chart A: Specific Energy Of Various Fuels

Fuel

Heat Value Btu/lb.

Stoichio. A/F

Pk. Pwr. A/F

SE (Stoichio.) Btu/lb. ÷  A/F

SE (Pk. Pwr. A/F)

Btu/lb. ÷ A/F

Gasoline

19,000

14.7/1

12.4/1

1293

1532

Methanol

8,500

6.45/1

4/1

1318

2125

Nitromethane

4,850

1.7/1

1/1

2853

4850

 

Like methanol, nitromethane is a substituted methane hydrocarbon (CH4), where a nitro group replaces one hydrogen atom (CH3NO2). Chemists refer to nitro (like methanol) as a partially oxidized fuel; the nitro molecule contains 52.2 percent oxygen by weight; methanol is 49.9 percent. At first glance, the two fuels appear to be about equal in terms of oxygen content. A closer examination reveals a different situation: the nitromethane molecule is 1.43 times denser than the methanol molecule (9.48 lb./gal ÷ 6.63 lb./gal = 1.43). When molecular densities are taken into consideration, nitromethane’s molecule is found to contain almost 50 percent more oxygen by weight than methanol; this explains why more nitro needs to be added to the engine’s inducted air at peak power air/fuel ratios than other fuels. Here are the calculations:

 

1.43 x 0.522 (%O2) = 0.746 = 1.49 (nitro)

 1 x 0.499 (%O2) = 0.499 1 (methanol)

 

(1.49 – 1) ÷ 1 = 0.49

 

Therefore, nitro’s significant oxygen content is largely responsible for it having 128 percent more specific energy (SE) than methanol at peak power A/F ratios (4850 – 2125) ÷ 2125 = 1.28.

 

REACTANTS AND PRODUCTS OF NEAT NITROMETHANE COMBUSTION

The performance of any fuel in an internal-combustion engine relates to its release of combustion energy, which can be modified by the dissociation of the combustion products. With more moles of combustion product, the product/reactants ratio is further enhanced, and this increases the engine’s indicated horsepower (cylinder hp) even further.

 

The balanced equation for nitromethane at its stoichiometric air/fuel ratio is: 4CH3NO2 + 3O2 → 4CO2 + 6H2O + 2N2. There are 12 moles of product and 7 moles of reactants from the above equation, forming a ratio of 12:7 (12-7) ÷7 = 0.71, or 71% more products than reactants. Compare this to methanol’s stoichiometric products/reactants ratio, which has only 20% more products than reactants, an indication of nitro’s potency.

Top-Fuel and Funny Cars never operate at (or near) stoichiometric air/fuel ratios; engine temperatures would climb beyond the melting point of its components. As the nitromethane mixture is richened toward its peak power air/fuel ratio, new combustion products are formed by dissociation, changing the products/reactants ratio for the better (e.g., at an air/fuel ratio of 1.13:1, nitro begins producing carbon monoxide [CO] in addition to CO2, H2O, and N2); this raises the molar ratio to 2:1 (100% more products than reactants). Further richening nitro’s mixture ratio to 0.75:1 produces another new product: hydrogen (H2); in this case, the molar products/reactants ratio improves to 18:8 (125% more products than reactants), almost four times that of methanol at its peak power air/fuel ratio (33% more products than reactants). If pure (neat) nitromethane is richened to the point where no inducted air is used on the reactants side of the molar product’s/reactant’s ratio (24:8 = 2.00 or 200% more products than reactants), it still might burn, much as it does inside the combustion chamber of a monopropellant rocket engine. This is why Top Fuel and Funny Cars shut-off the fuel as well as the ignition at the end of each pass; otherwise, the engine often refuses to stop running. Large molar product/reactant ratios, coupled with an extremely high specific energy, make nitromethane a powerful and unique fuel.

 

NITROMETHANE – LATENT HEAT OF VAPORIZATION COOLING

Contrary to popular belief nitromethane (theoretically) has an engine-cooling advantage over other fuels due to two factors: its fuel rich air/fuel ratio and its latent heat of vaporization. Latent heat of vaporization is defined as the amount of heat energy required for a substance to change state; in this case, from a liquid (at its boiling point temperature) to a gas. Although methanol requires more heat per pound to vaporize (472 to 258 Btu/lb.), nitro’s high fuel flow rate more than compensates. When these two factors are taken into account, nitro’s cooling effect is about twice that of methanol. See Chart B.

 

Chart B: Latent Heat Of Vaporization Cooling

Fuel

Heat of Vapor Btu/lb.

Stoichio. A/F

Pk. Pwr. A/F

Heat of Vapor÷Stoichio. A/F

Heat of Vapor÷Pk. Pwr. A/F

Gasoline

135

14.7/1

12.4/1

9.2

10.9

Methanol

472

6.45/1

4.0/1

73.2

118

Nitromethane

258

1.7/1

1/1

151.8

258

 

Unfortunately, only a small percentage of nitro’s vaporization-cooling potential is ever realized. In comparison, removing heat from a liquid without changing state is known as sensible heat, and is many times less effective than latent heat for any given liquid. In drag racing, where extremely rich, near-neat nitromethane mixtures are used to control combustion temperatures and detonation, vaporization cooling is ignored, thrown to the wolves. Only part of nitromethane’s fuel charge is atomized (a liquid that has been broken into small particles), let alone vaporized in its flood-like rush to the combustion chamber and beyond. Conduction, a sensible heat removal process, provides most of the cooling between the engine’s components and the liquid nitro.

 

PHYSICAL PROPERTIES – NITROMETHANE

Flash point - 112º F

Boiling point - 214º F

Vapor pressure at 20º C – 0.54 psi

Specific gravity – 1.139 at 60º F

Weight – 9.48 lb./gal (U.S.)

Auto ignition temperature - 785º F
Comments:
Tuesday, June 30, 2009 9:27:01 PM by Anonymous
Very interesting technical article about NitroMethane.

You mention, "These were the golden years of fuel-stock availability." That is when using benzene and propylene oxide.

Those were naive years when we didn't know about the cancer causing effect of benzene, now propylene oxide, and now nitromethane that has been listed as a possible cause of cancer.

We should be more careful with nitro containing fuels and avoid breathing vapours and wear disposable gloves to avoid contact.

http://www.nrcan-rncan.gc.ca/com/elements/issues/25/precurs-eng.php

http://www.chemicalsubstanceschimiques.gc.ca/challenge-defi/batch-lot-8/info_e.html

Bob Long

Leave your comment
 
Choose an identity
Blogger Other Anonymous
 
Username 
Password 
No Blogger account? Sign up here.
CAPTCHA Validation
Retype the code from the picture
CAPTCHA Code Image
Speak the code Change the code
 

Search:








Subscribe |  RCStore |  Privacy Policy | Terms of UseAdvertising | Contact Us

Copyright © 2010 Model Airplane News All rights reserved.  | Console Login