Knock-limited peformance of blends of AN-F-28 fuel containing 2 percent aromatic amines - 2 / by Henry E. Alquist and Leonard K. Tower.

Tests were conducted to investigate the effect of 2-percent additions of nine aromatic amines on the knock-limited performance of AN-F-28 (28-R) fuel. Knock tests were made on nine aromaitic amines synthesized, or purchased and purified, at the Aircraft Engine Research Laboratory.

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Bibliographic Details
Main Author:	Alquist, Henry E.
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Aircraft Engine Research Laboratory
Other Authors:	Tower, Leonard K.
Other title:	NACA Wartime Reports. Series E.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. E149.
Subjects:	Airplanes > Fuel. Motor fuels > Anti-knock and anti-knock mixtures. Aromatic amines.

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The effect of liquid and ice particles on the erosion of a supercharger-inlet cover and diffuser vanes / by Rollin, Vern Gordon

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Efficiency of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip diameter / by Coulter, Earl E.

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An evaluation of the knock-limited performance of triptane / by Barnett, Henry C.

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Investigation of ice formation in the induction system of an aircraft engine. : 1 - Ground tests / by Essex, Henry A.

Published 1946

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Knock-limited peformance of blends of AN-F-28 fuel containing 2 percent aromatic amines - 2 / by Henry E. Alquist and Leonard K. Tower.

Aerodynamics of the carburetor air scoop and the engine cowling of a single-engine torpedo-bomber-type airplane / by Kuenzig, John K.

Air-flow and performance characteristics of engine-stage supercharger of a double-row radial aircraft engine. : 2 - Effect of design variables / by Baas, Edmund J.

Altitude-wind-tunnel tests of power-plant installation in jet-propelled fighter / by Preston, G. Merritt

Analysis of cooling limitations and effect of engine-cooling improvements on level-flight cruising performance of a four-engine heavy bomber / by Marble, Frank E.

Analysis of spark-ignition engine knock as seen in photographs taken at 200,000 frames a second / by Miller, Cearcy D.

Charge-air distribution among the cylinders of a double-row radial aircraft engine / by Guentert, Donald G.

Correlation of mixture temperature data obtained from bare intake-manifold thermocouples / by White, H. Jack

A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine - 2 / by Alquist, Henry E.

Determination of gas temperatures from the frequency of knock-induced gas vibrations in an internal-combustion engine / by Moeckel, W. E. (Wolfgang E.)

Effect of a low-loss air valve on performance of a 22-inch-diameter pulse-jet engine / by Bressman, Joseph R.

The effect of ethylene dibromide on the knock-limited performance of leaded and nonleaded S reference fuel / by Kinney, George R.

The effect of increase in combustion-air inlet temperature from 80 to 130 degrees F on the sea-level performance of a 22-inch-diameter pulse-jet engine / by Valerino, Michael F.

The effect of liquid and ice particles on the erosion of a supercharger-inlet cover and diffuser vanes / by Rollin, Vern Gordon

Effects of fuel-vapor loss on knock-limited performance and inspection properties of aviation fuels / by Barnett, Henry C.

Efficiency of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip diameter / by Coulter, Earl E.

An evaluation of the knock-limited performance of triptane / by Barnett, Henry C.

Hydraulic characteristics of the NACA injection impeller / by Ritter, William K.

An investigation of cowl-flap and cowl-outlet designs for the B-29 power-plant installation / by Wyatt, DeMarquis D.

An investigation of cowl inlets for the B-29 power-plant installation / by Monroe, Louis L.

Investigation of ice formation in the induction system of an aircraft engine. : 1 - Ground tests / by Essex, Henry A.

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