The NASA High-speed Turboprop Program

The NASA High-speed Turboprop Program
Author: James F. Dugan
Publisher:
Total Pages: 24
Release: 1980
Genre: Aircraft cabins
ISBN:


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"NASAs Advanced Turboprop Project is a three phased effort initiated in 1978 to provide technology readiness for Mach 0.7 to 0.8 turboprop-powered aircraft with the potential for fuel savings and DOC reductions of up to 30 and 15 percent respectively relative to current in-service aircraft. This paper reviews the status of Phase I in the areas of propeller aeroacoustics, propeller structures, turboprop installed performance, aircraft cabin environment, and turboprop engine and aircraft studies. Current plans to establish large-scale propeller characteristics and to conduct high-speed propeller flight research tests using a modified testbed aircraft are also presented.--Report documentation page.


The NASA High-speed Turboprop Program
Language: en
Pages: 24
Authors: James F. Dugan
Categories: Aircraft cabins
Type: BOOK - Published: 1980 - Publisher:

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"NASAs Advanced Turboprop Project is a three phased effort initiated in 1978 to provide technology readiness for Mach 0.7 to 0.8 turboprop-powered aircraft with
Advanced Turboprop Project
Language: en
Pages: 140
Authors: Roy D. Hager
Categories: Airplanes
Type: BOOK - Published: 1988 - Publisher:

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The Power for Flight
Language: en
Pages: 318
Authors: Jeremy R. Kinney
Categories: Airplanes
Type: BOOK - Published: 2018-02-15 - Publisher: Government Printing Office

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The NACA and aircraft propulsion, 1915-1958 -- NASA gets to work, 1958-1975 -- The shift toward commercial aviation, 1966-1975 -- The quest for propulsive effic
Advanced Turboprop Project
Language: en
Pages: 130
Authors: Roy D. Hager
Categories: Airplanes
Type: BOOK - Published: 1988 - Publisher:

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The Theory of Propellers
Language: en
Pages: 184
Authors: Theodore Theodorsen
Categories: Aerodynamics
Type: BOOK - Published: 1944 - Publisher:

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Summary: A technical method is given for calculating the axial interference velocity of a propeller. The method involves the use of certain weight functions P,