Knock-limited Performance of Pure Hydrocarbons Blended with a Base Fuel in a Full-scale, Aircraft-engine Cylinder

Knock-limited Performance of Pure Hydrocarbons Blended with a Base Fuel in a Full-scale, Aircraft-engine Cylinder PDF Author: Anthony W. Jones
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20

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Book Description
Knock-limited performance tests of leaded blends of four pure aromatic hydrocarbons and six pure ethers with a base fuel were conducted in a full-scale aircraft-engine cylinder at two operating conditions to determine the antiknock effectiveness of additions of pure compounds to aviation fuels.

Knock-limited Performance of Pure Hydrocarbons Blended with a Base Fuel in a Full-scale, Aircraft-engine Cylinder

Knock-limited Performance of Pure Hydrocarbons Blended with a Base Fuel in a Full-scale, Aircraft-engine Cylinder PDF Author: Anthony W. Jones
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20

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Book Description
Knock-limited performance tests of leaded blends of four pure aromatic hydrocarbons and six pure ethers with a base fuel were conducted in a full-scale aircraft-engine cylinder at two operating conditions to determine the antiknock effectiveness of additions of pure compounds to aviation fuels.

The Knock-limited Performance of Fuel Blends Containing Aromatics

The Knock-limited Performance of Fuel Blends Containing Aromatics PDF Author: Carl L. Meyer
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50

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Book Description
Results are reported of knock-limited tests of five aromatics, each individually blended with selected base fuels and tested with and without TEL, using 17.6, F-4, and F-3 small-scale engines. The five aromatics rated in the following order of decreasing antiknock effectiveness at fuel/air ratio 0.10: m-xylene, 1-isopropyl-4-methylbenzene, n-propylbenzene, isobutylbenzene, and n-butylbenzene.

Knock-limited Performance Tests of 2,2,3,4-tetramethylpentane, 2,3,3,4-tetramethylpentane, 3,4,4-trimethyl-2-pentene, and 2,3,4-trimethyl-2-pentene in Small-scale and Full-scale Cylinders

Knock-limited Performance Tests of 2,2,3,4-tetramethylpentane, 2,3,3,4-tetramethylpentane, 3,4,4-trimethyl-2-pentene, and 2,3,4-trimethyl-2-pentene in Small-scale and Full-scale Cylinders PDF Author: Edmund R. Jonash
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

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Book Description
Knock-limited tests were conducted with F-4, F-3, and 17.6 small-scale engines and with a full-scale cylinder on blends containing the following purified hydrocarbons: 2,2,3,4-tetramethylpentane, 2,3,3,4-tetramethylpentane, 3,4,4-trimethyl-2-pentene, and 2,3,4-trimethyl-2-pentene.

Wartime Report

Wartime Report PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 342

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Wartime Report E.

Wartime Report E. PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 270

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Knock-limited Performance of Several Branched Paraffins and Olefins

Knock-limited Performance of Several Branched Paraffins and Olefins PDF Author: R. S. Genco
Publisher:
ISBN:
Category : Alkanes
Languages : en
Pages : 46

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Book Description
At mild or moderate engine severity, 2,2,3,3-tetramethylpentane blend was highest in knock limit of the paraffins tested, but at severe conditions it was lowest; at severe (F-3) conditions, triptane blend was best.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 374

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Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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