Heat-transfer tests of a steel cylinder barrel with aluminum fins of optimum proportions / by Herman H. Ellerbrock, Jr., and Alvin H. Mann.

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Bibliographic Details
Main Author:	Ellerbrock, Herman H.
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Aircraft Engine Research Laboratory
Other Authors:	Mann, Alvin H.
Other title:	NACA Wartime Reports. Series E.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1940]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. E204.
Subjects:	Airplanes > Motors > Cylinders. Internal combustion engines > Cylinders. Airplanes > Motors > Cooling. Heat > Transmission. Aluminum. Charts, diagrams, etc.

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

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

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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.

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

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

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

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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.

Published 1946

Search for the full-text version of this title in HathiTrust

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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

Published 1946

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

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

Published 1946

Search for the full-text version of this title in HathiTrust

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

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

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

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

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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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Heat-transfer tests of a steel cylinder barrel with aluminum fins of optimum proportions / by Herman H. Ellerbrock, Jr., and Alvin H. Mann.

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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