Explore: Propulsive Efficiency
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Books Results
Source: The Open Library
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Search results from The Open Library
1Physics & Process Modeling (PPM) and Other Propulsion R&T
By PPM and Other Propulsion R & T Conference (1997 Cleveland, Ohio)
“Physics & Process Modeling (PPM) and Other Propulsion R&T” Metadata:
- Title: ➤ Physics & Process Modeling (PPM) and Other Propulsion R&T
- Author: ➤ PPM and Other Propulsion R & T Conference (1997 Cleveland, Ohio)
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Physics & Process Modeling (PPM) and Other Propulsion R&T” Subjects and Themes:
- Subjects: ➤ Refractory materials - Engine parts - Propulsive efficiency - Propulsion system performance - Hybrid propulsion - Propulsion systems - Engines - Space vehicles
Edition Identifiers:
- The Open Library ID: OL17137042M - OL17593506M - OL18138784M - OL15561022M - OL22404377M
- Online Computer Library Center (OCLC) ID: 43269447
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
By Daniel J. Dorney
“Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Metadata:
- Title: ➤ Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
- Author: Daniel J. Dorney
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Subjects and Themes:
- Subjects: ➤ Blade-vortex interaction - Navier-Stokes equation - Propulsive efficiency - Reynolds number - Rotor stator interactions - Turbine blades - Turbines - Unsteady aerodynamics - Unsteady flow - Wakes
Edition Identifiers:
- The Open Library ID: OL17546454M - OL18116215M - OL17123448M - OL15491903M
- Online Computer Library Center (OCLC) ID: 39109525
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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3Metallized gelled propellants
By Bryan A. Palaszewski
“Metallized gelled propellants” Metadata:
- Title: Metallized gelled propellants
- Author: Bryan A. Palaszewski
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995 - 1996 - 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - [Washington, D.C - Springfield, Va
“Metallized gelled propellants” Subjects and Themes:
- Subjects: ➤ Heat flux - Heat transfer - Metal combustion - Liquid rocket propellants - Rocket engines - Gelled propellants - Metal propellants - Propellant combustion - Propellant additives - Flux quantization - Aluminum - Hydrocarbon fuels - Specific impulse - Temperature profiles - Gelled rocket propellants - Oxygen - Calorimeters - Propulsive efficiency - Propulsion system performance - Heat measurement
Edition Identifiers:
- The Open Library ID: OL17131208M - OL17125103M - OL15420743M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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4Ultra-efficient engine diameter study
By D. L. Daggett
“Ultra-efficient engine diameter study” Metadata:
- Title: ➤ Ultra-efficient engine diameter study
- Author: D. L. Daggett
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA - Hanover, MD
“Ultra-efficient engine diameter study” Subjects and Themes:
- Subjects: ➤ Mass flow rate - Turbofans - Turbofan engines - Jet flow - Propulsive efficiency - Bypass ratio
Edition Identifiers:
- The Open Library ID: OL16094181M - OL17633156M - OL18205106M
- Online Computer Library Center (OCLC) ID: 56823361
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5Current wind tunnel capability and planned improvements at Lewis Research Center
By David N. Bowditch
“Current wind tunnel capability and planned improvements at Lewis Research Center” Metadata:
- Title: ➤ Current wind tunnel capability and planned improvements at Lewis Research Center
- Author: David N. Bowditch
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Current wind tunnel capability and planned improvements at Lewis Research Center” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Anechoic chambers - Engine noise - Lewis Research Center - Mach number - Propulsion system performance - Propulsive efficiency - Simulation - Supersonic wind tunnels - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17727145M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Advanced Rotorcraft Transmission (ART) Program
By Joseph W. Lenski
“Advanced Rotorcraft Transmission (ART) Program” Metadata:
- Title: ➤ Advanced Rotorcraft Transmission (ART) Program
- Author: Joseph W. Lenski
- Language: English
- Publisher: ➤ For sale by the National Technical information Service - National Aeronautics and Space Administration - US Army Aviation Systems Command, Aviation R&T Activity
- Publish Date: 1991
- Publish Location: ➤ [St. Louis, Mo.] - [Washington, DC] - [Springfield, Va
“Advanced Rotorcraft Transmission (ART) Program” Subjects and Themes:
- Subjects: ➤ Transmissions (Machine elements) - Helicopter propeller drive - Gears - Propulsive efficiency - Bearings - Service life
Edition Identifiers:
- The Open Library ID: OL15406157M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7Propulsion over a wide Mach number range
By Edwin L. Resler
“Propulsion over a wide Mach number range” Metadata:
- Title: ➤ Propulsion over a wide Mach number range
- Author: Edwin L. Resler
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Cornell University
- Publish Date: 1989
- Publish Location: ➤ Ithaca, NY - Springfield, Va - [Washington, DC
“Propulsion over a wide Mach number range” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15407413M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Independent Orbiter assessment
By P. S. Bailey
“Independent Orbiter assessment” Metadata:
- Title: Independent Orbiter assessment
- Author: P. S. Bailey
- Language: English
- Publisher: ➤ McDonnell Douglas Astronautics Company, Houston Division - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: Houston, Tex - [Washington, DC
“Independent Orbiter assessment” Subjects and Themes:
- Subjects: ➤ Controllers - Space shuttle orbiters - Failure modes - Spacecraft reliability - Propulsive efficiency - Manned maneuvering units - Manned maneuvering units (Space flight)
Edition Identifiers:
- The Open Library ID: OL18263649M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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9Operating characteristics of the Russian D-55 thruster with anode layer
By John M. Sankovic
“Operating characteristics of the Russian D-55 thruster with anode layer” Metadata:
- Title: ➤ Operating characteristics of the Russian D-55 thruster with anode layer
- Author: John M. Sankovic
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Operating characteristics of the Russian D-55 thruster with anode layer” Subjects and Themes:
- Subjects: ➤ . - Electromagnets - Thrust measurement - Propulsive efficiency - Specific impulse - Electric propulsion - Propulsion system performance - Rocket engines
Edition Identifiers:
- The Open Library ID: OL15401820M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10Energy efficient engine program
By David C. Howe
“Energy efficient engine program” Metadata:
- Title: ➤ Energy efficient engine program
- Author: David C. Howe
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Energy efficient engine program” Subjects and Themes:
- Subjects: Gas turbine engines - Engine tests - Design analysis - Engine design - Propulsive efficiency
Edition Identifiers:
- The Open Library ID: OL15402413M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Application of computational fluid dynamics in high speed aeropropulsion
By Louis A. Povinelli
“Application of computational fluid dynamics in high speed aeropropulsion” Metadata:
- Title: ➤ Application of computational fluid dynamics in high speed aeropropulsion
- Author: Louis A. Povinelli
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1991
- Publish Location: [Cleveland, Ohio
“Application of computational fluid dynamics in high speed aeropropulsion” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aircraft engines - Propulsive efficiency - Flow distribution - Propulsion system performance - Hypersonic flight
Edition Identifiers:
- The Open Library ID: OL16130460M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Propulsive efficiency
the propulsive efficiency is expressed as the proportion of the mechanical energy actually used to propel the aircraft. The propulsive efficiency is always
Turbofan
stages Overall efficiency thermal efficiency × propulsive efficiency Propulsive efficiency propulsive power/rate of production of propulsive kinetic energy
Jet aircraft
less-than-ideal efficiency of the propulsive mechanism, whether a propeller, a jet exhaust, or a fan. In addition, propulsive efficiency is greatly dependent
Fuel economy in aircraft
weight, and with improved engine brake-specific fuel consumption and propulsive efficiency or thrust-specific fuel consumption. Endurance and range can be
Jet engine
In addition to propulsive efficiency, another factor is cycle efficiency; a jet engine is a form of heat engine. Heat engine efficiency is determined by
Ion thruster
20–50 km/s (Isp 2000–5000 s), and possess thrusts of 25–250 mN and a propulsive efficiency 65–80% though experimental versions have achieved 100 kW (130 hp)
Ramjet
Aviation Week (6 February 1950). Aviation Week 1950-02-06. p. 22. "Propulsive Efficiency from an Energy Utilization Standpoint". The Cornell Engineer. 16
Bypass ratio
unducted fan installations because their high propulsive efficiency gives them the overall efficiency characteristics of very high bypass turbofans.
Reaction engine
the exhaust stops in space and has no kinetic energy; and the propulsive efficiency is 100% all the energy ends up in the vehicle (in principle such
Turboprop
Wayback Machine Prof. Z. S. Spakovszky. "11.5 Trends in thermal and propulsive efficiency" MIT turbines, 2002. Thermodynamics and Propulsion Hall, Nancy (2021)