Explore: Propulsive Efficiency
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Books Results
Source: The Open Library
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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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