Explore: Aircraft Configurations
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Source: The Open Library
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1High-speed research
By High Speed Research Program Sonic Boom Workshop (3rd 1994 Langley Research Center)
“High-speed research” Metadata:
- Title: High-speed research
- Author: ➤ High Speed Research Program Sonic Boom Workshop (3rd 1994 Langley Research Center)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“High-speed research” Subjects and Themes:
- Subjects: ➤ Aircraft configurations - Conferences - Design and construction - High-speed aeronautics - Sonic boom - Sonic booms - Space vehicles - Supersonic Aerodynamics - Supersonic flight - Congresses
Edition Identifiers:
- The Open Library ID: ➤ OL18140481M - OL15571721M - OL18296438M - OL22402556M - OL17595624M - OL14510231M
- Online Computer Library Center (OCLC) ID: 44569471
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Low-speed wind tunnel tests of two waverider configuration models
By Robert J. Pegg
“Low-speed wind tunnel tests of two waverider configuration models” Metadata:
- Title: ➤ Low-speed wind tunnel tests of two waverider configuration models
- Author: Robert J. Pegg
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Low-speed wind tunnel tests of two waverider configuration models” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Directional stability - Lift drag ratio - Wind tunnel tests - Aircraft configurations - Subsonic speed - Aerodynamic stability - Angle of attack - Pitching moments - Waveriders - Lateral stability - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17565252M - OL18118663M - OL15498353M - OL17124624M
- Online Computer Library Center (OCLC) ID: 39554715
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Dual-mission large aircraft feasibility study and aerodynamic investigation
By Dimitri Mavris
“Dual-mission large aircraft feasibility study and aerodynamic investigation” Metadata:
- Title: ➤ Dual-mission large aircraft feasibility study and aerodynamic investigation
- Author: Dimitri Mavris
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Dual-mission large aircraft feasibility study and aerodynamic investigation” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Feasibility analysis - Civil aviation - Transport aircraft - Cost analysis - Air transportation - Aircraft configurations
Edition Identifiers:
- The Open Library ID: OL17575887M - OL18131608M - OL17127521M - OL15538168M
- Online Computer Library Center (OCLC) ID: 40556387
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Development of a computer program for analyzing preliminary aircraft configurations in relationship to emerging agility metrics
By Brent Alan Bauer
“Development of a computer program for analyzing preliminary aircraft configurations in relationship to emerging agility metrics” Metadata:
- Title: ➤ Development of a computer program for analyzing preliminary aircraft configurations in relationship to emerging agility metrics
- Author: Brent Alan Bauer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Development of a computer program for analyzing preliminary aircraft configurations in relationship to emerging agility metrics” Subjects and Themes:
- Subjects: Technology utilization - Aircraft design - Aircraft configurations - Computer aided design - Computer programs
Edition Identifiers:
- The Open Library ID: OL17837371M - OL17697881M - OL18121954M
- Online Computer Library Center (OCLC) ID: 40147945
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
By Guy T. Kemmerly
“Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” Metadata:
- Title: ➤ Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
- Author: Guy T. Kemmerly
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - Hampton, Va - [Washington, D.C.]
“Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Short takeoff aircraft - Aircraft landing - Ground effect (Aerodynamics) - Aircraft configurations - Landing - Aerodynamic characteristics - Ground effect - Ground tests
Edition Identifiers:
- The Open Library ID: OL18257141M - OL20268762M - OL16135235M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6An edge-based solution-adaptive method applied to the AIRPLANE code
By Rupak Biswas
“An edge-based solution-adaptive method applied to the AIRPLANE code” Metadata:
- Title: ➤ An edge-based solution-adaptive method applied to the AIRPLANE code
- Author: Rupak Biswas
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, CA]
“An edge-based solution-adaptive method applied to the AIRPLANE code” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Transonic flow - Near fields - Unstructured grids (Mathematics) - Flow distribution - Aircraft configurations - Sonic booms - Grid generation (Mathematics) - Supersonic flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL15419501M - OL18084638M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7HOMAR:a computer code for generating homotopic grids using algebraic relations
By Anutosh Moitra
“HOMAR:a computer code for generating homotopic grids using algebraic relations” Metadata:
- Title: ➤ HOMAR:a computer code for generating homotopic grids using algebraic relations
- Author: Anutosh Moitra
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“HOMAR:a computer code for generating homotopic grids using algebraic relations” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft configurations - Applications programs (Computers) - Body-wing configurations - Computational geometry - Computational grids - Computer systems programs - Grid generation (Matematics) - Homotopy theory
Edition Identifiers:
- The Open Library ID: OL14972278M - OL17683520M
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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8A modeling technique for STOVL ejector and volume dynamics
By Colin K. Drummond
“A modeling technique for STOVL ejector and volume dynamics” Metadata:
- Title: ➤ A modeling technique for STOVL ejector and volume dynamics
- Author: Colin K. Drummond
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“A modeling technique for STOVL ejector and volume dynamics” Subjects and Themes:
- Subjects: ➤ Mathematical models - Jet propulsion - Short take-off and landing aircraft - Ejectors - Computational fluid dynamics - V/STOL aircraft - Aircraft configurations - Performance prediction - Thrust
Edition Identifiers:
- The Open Library ID: OL17634486M - OL16132181M
- Online Computer Library Center (OCLC) ID: 25053445
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9The design of a high capacity long range cargo aircraft
By Terry A. Weisshaar
“The design of a high capacity long range cargo aircraft” Metadata:
- Title: ➤ The design of a high capacity long range cargo aircraft
- Author: Terry A. Weisshaar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Purdue University, School of Aeronauticss and Astronautics
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - West Lafayette, Ind - [Washington, DC
“The design of a high capacity long range cargo aircraft” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Freight costs - Cargo aircraft - Air cargo - Aircraft design - Aircraft configurations - Cost reduction
Edition Identifiers:
- The Open Library ID: OL15403004M - OL17790176M
- Online Computer Library Center (OCLC) ID: 32174199
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10A users manual for the method of moments Aircraft Modeling Code (AMC)
By M. E. Peters
“A users manual for the method of moments Aircraft Modeling Code (AMC)” Metadata:
- Title: ➤ A users manual for the method of moments Aircraft Modeling Code (AMC)
- Author: M. E. Peters
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering
- Publish Date: 1989 - 1994
- Publish Location: ➤ Hampton, Va - [Springfield, Va - Columbus, Ohio - [Springfield, VA - Hampton, VA
“A users manual for the method of moments Aircraft Modeling Code (AMC)” Subjects and Themes:
- Subjects: ➤ User manuals (Computer programs) - Aircraft configurations - Method of moments - Command languages - Electromagnetic scattering - Geometry - Computer programs - Applications programs (Computers) - Shapes - Antenna radiation patterns
Edition Identifiers:
- The Open Library ID: OL15403998M - OL16127039M
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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11Supersonic flow computations for an ASTOVL aircraft configuration
By Sekaripuram Ramakrishnan
“Supersonic flow computations for an ASTOVL aircraft configuration” Metadata:
- Title: ➤ Supersonic flow computations for an ASTOVL aircraft configuration
- Author: Sekaripuram Ramakrishnan
- Language: English
- Number of Pages: Median: 40
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - Hampton, Va
“Supersonic flow computations for an ASTOVL aircraft configuration” Subjects and Themes:
- Subjects: ➤ Supersonic flow - Computational fluid dynamics - Short takeoff aircraft - Grid generation (Mathematics) - Aircraft configurations - V/STOL aircraft - Design analysis
Edition Identifiers:
- The Open Library ID: OL16135381M - OL20268695M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
By Lawrence R. Reardon
“Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature” Metadata:
- Title: ➤ Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
- Author: Lawrence R. Reardon
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - Springfield, VA
“Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature” Subjects and Themes:
- Subjects: ➤ Testing - Strain gages - Low aspect ratio wings - Aircraft structures - Calibration - Load tests - High temperatures - Wing loading - Aircraft configurations - Calibrating - Airplanes - High temperature environments - Airframes - Wings
Edition Identifiers:
- The Open Library ID: OL16123561M - OL18225827M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport
By Louis J. Glaab
“Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport” Metadata:
- Title: ➤ Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport
- Author: Louis J. Glaab
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport” Subjects and Themes:
- Subjects: ➤ Pilot support systems - Computerized simulation - Takeoff - Noise intensity - Aerodynamic noise - Aircraft configurations - Noise prediction (Aircraft) - Noise reduction - Lift
Edition Identifiers:
- The Open Library ID: OL15569357M
- Online Computer Library Center (OCLC) ID: 44447728
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Advanced Rotorcraft Transmission Program
By Robert C. Bill
“Advanced Rotorcraft Transmission Program” Metadata:
- Title: ➤ Advanced Rotorcraft Transmission Program
- Author: Robert C. Bill
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1990
- Publish Location: [Cleveland, Ohio
“Advanced Rotorcraft Transmission Program” Subjects and Themes:
- Subjects: ➤ Helicopter design - Helicopter propeller drive - Mechanical drives - Aircraft configurations - Rotary wing aircraft - Transmissions (Machine elements) - Noise reduction - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL16131237M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
By Nicholas J. Georgiadis
“Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system” Metadata:
- Title: ➤ Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
- Author: Nicholas J. Georgiadis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system” Subjects and Themes:
- Subjects: ➤ Aircraft configurations - Computational fluid dynamics - Ejectors - K-epsilon turbulence model - Multigrid methods - Navier-Stokes equation - Propulsion system configurations - Propulsion system performance - Ramjet engines - Supersonic combustion ramjet engines - Turbulent mixing - Two dimensional flow
Edition Identifiers:
- The Open Library ID: OL15550614M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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16Tailless aircraft performance improvements
By Irving Louis Ashkenas
“Tailless aircraft performance improvements” Metadata:
- Title: ➤ Tailless aircraft performance improvements
- Author: Irving Louis Ashkenas
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va - [Springfield, Va
“Tailless aircraft performance improvements” Subjects and Themes:
- Subjects: ➤ Aircraft configurations - Aircraft control - Aircraft performance - Remotely piloted Vehicles - Static stability - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15407752M
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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17Portable parallel stochastic optimization for the design of aeropropulsion components
By Robert Henry Sues
“Portable parallel stochastic optimization for the design of aeropropulsion components” Metadata:
- Title: ➤ Portable parallel stochastic optimization for the design of aeropropulsion components
- Author: Robert Henry Sues
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Applied Research Associates, Inc. - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Raleigh, N.C - [Washington, DC
“Portable parallel stochastic optimization for the design of aeropropulsion components” Subjects and Themes:
- Subjects: ➤ Architecture (Computers) - Parallel programming - Stochastic processes - Massively parallel processors - Computer techniques - Aircraft configurations - Aircraft engines - Parallel processing (Computers) - Design analysis - Multiprocessing (Computers) - Programming environments - Optimization
Edition Identifiers:
- The Open Library ID: OL15408454M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Investigation into the impact of agility in conceptual fighter design
By R. M. Engelbeck
“Investigation into the impact of agility in conceptual fighter design” Metadata:
- Title: ➤ Investigation into the impact of agility in conceptual fighter design
- Author: R. M. Engelbeck
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Investigation into the impact of agility in conceptual fighter design” Subjects and Themes:
- Subjects: ➤ Maneuverability - Fighter aircraft - Technology assessment - Aircraft design - Aircraft configurations - Flight characteristics - Design analysis
Edition Identifiers:
- The Open Library ID: OL15419852M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Flight simulation software at NASA Dryden Flight Research Center
By Ken A. Norlin
“Flight simulation software at NASA Dryden Flight Research Center” Metadata:
- Title: ➤ Flight simulation software at NASA Dryden Flight Research Center
- Author: Ken A. Norlin
- Language: English
- Publisher: ➤ Available from the NASA Center for AeroSpace Information - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1995
- Publish Location: ➤ [Linthicum Heights, MD - Edwards, Calif - Springfield, Va
“Flight simulation software at NASA Dryden Flight Research Center” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Flight simulation - Real time operation - UNIX (Operating system) - Aircraft configurations - Applications programs (Computers) - Software engineering - Fixed wings
Edition Identifiers:
- The Open Library ID: OL15420778M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
By Charles W. Boppe
“Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds” Metadata:
- Title: ➤ Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Author: Charles W. Boppe
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1987
- Publish Location: [Washington, D.C.]
“Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds” Subjects and Themes:
- Subjects: ➤ Aircraft structures - Computational grids - Transonic flow - Aerodynamics - Aircraft design - Aircraft configurations - Aerodynamic interference
Edition Identifiers:
- The Open Library ID: OL16122225M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
By R. A. Hess
“Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” Metadata:
- Title: ➤ Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
- Author: R. A. Hess
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, VA
“Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” Subjects and Themes:
- Subjects: ➤ Controllability - Frequency ranges - Aircraft control - Pilot induced oscillation - Actuators - Aircraft pilots - Aircraft configurations
Edition Identifiers:
- The Open Library ID: OL17837927M
- Online Computer Library Center (OCLC) ID: 40660562
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
By R. A. Hess
“Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” Metadata:
- Title: ➤ Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
- Author: R. A. Hess
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, VA
“Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling” Subjects and Themes:
- Subjects: ➤ Controllability - Frequency ranges - Aircraft control - Pilot induced oscillation - Actuators - Aircraft pilots - Aircraft configurations
Edition Identifiers:
- The Open Library ID: OL15543294M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions
By Louis J. Glaab
“Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions” Metadata:
- Title: ➤ Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions
- Author: Louis J. Glaab
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions” Subjects and Themes:
- Subjects: ➤ Control theory - Flight control - Civil aviation - Flight simulation - Aircraft configurations - Supersonic transports - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15564668M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Supersonic civil airplane study and design
By Samson H. Cheung
“Supersonic civil airplane study and design” Metadata:
- Title: ➤ Supersonic civil airplane study and design
- Author: Samson H. Cheung
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va - [Washington, DC
“Supersonic civil airplane study and design” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Computational fluid dynamics - Aircraft configurations - Computer aided design - Sonic booms - Aerodynamic configurations - Aircraft design - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15413728M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25Integrated flight and propulsion controls for advanced aircraft configurations
By Walter C. Merrill
“Integrated flight and propulsion controls for advanced aircraft configurations” Metadata:
- Title: ➤ Integrated flight and propulsion controls for advanced aircraft configurations
- Author: Walter C. Merrill
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Integrated flight and propulsion controls for advanced aircraft configurations” Subjects and Themes:
- Subjects: Propulsion - Flight control - Aircraft configurations - Aircraft control - Engine control
Edition Identifiers:
- The Open Library ID: OL15420847M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Aerodynamic shape optimization of a HSCT type configuration with improved surface definition
By A. M. Thomas
“Aerodynamic shape optimization of a HSCT type configuration with improved surface definition” Metadata:
- Title: ➤ Aerodynamic shape optimization of a HSCT type configuration with improved surface definition
- Author: A. M. Thomas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Old Dominion University Research Foundation
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va - Norfolk, VA
“Aerodynamic shape optimization of a HSCT type configuration with improved surface definition” Subjects and Themes:
- Subjects: ➤ Computational geometry - Aircraft configurations - Aerospace vehicles - Grid generation (Mathematics) - Computer aided design - Aerodydnamic configurations - Aircraft design - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15408145M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Aeroelasticity of wing and wing-body configurations on parallel computers
By Chansup Byun
“Aeroelasticity of wing and wing-body configurations on parallel computers” Metadata:
- Title: ➤ Aeroelasticity of wing and wing-body configurations on parallel computers
- Author: Chansup Byun
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - San Jose, CA - [Washington, DC
“Aeroelasticity of wing and wing-body configurations on parallel computers” Subjects and Themes:
- Subjects: ➤ Parallel computers - Body-wing configurations - Aircraft configurations - Parallel processing (Computers) - Computer aided design - Aerodynamic configurations - Aeroelasticity - Aircraft design - Flutter
Edition Identifiers:
- The Open Library ID: OL15413748M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Some buffet response characteristics of a twin-vertical-tail configuration
By Stanley R. Cole
“Some buffet response characteristics of a twin-vertical-tail configuration” Metadata:
- Title: ➤ Some buffet response characteristics of a twin-vertical-tail configuration
- Author: Stanley R. Cole
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Some buffet response characteristics of a twin-vertical-tail configuration” Subjects and Themes:
- Subjects: ➤ Stabilizers (Fluid dynamics) - Stiffness - Buffeting - Wind tunnel tests - Aircraft configurations - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15405530M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29A user's manual for ROTTILT solver
By Hormoz Tadghighi
“A user's manual for ROTTILT solver” Metadata:
- Title: ➤ A user's manual for ROTTILT solver
- Author: Hormoz Tadghighi
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“A user's manual for ROTTILT solver” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - User manuals (Computer programs) - Rotors - Aircraft configurations - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15548903M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas
By Robert J. Mack
“A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas” Metadata:
- Title: ➤ A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas
- Author: Robert J. Mack
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas” Subjects and Themes:
- Subjects: ➤ Fuselages - Aircraft design - Force distribution - Sonic booms - Aircraft configurations - Mach number
Edition Identifiers:
- The Open Library ID: OL15405581M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Automatic procedures for computing complete configuration geometry for individual component descriptions
By Raymond L. Barger
“Automatic procedures for computing complete configuration geometry for individual component descriptions” Metadata:
- Title: ➤ Automatic procedures for computing complete configuration geometry for individual component descriptions
- Author: Raymond L. Barger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Automatic procedures for computing complete configuration geometry for individual component descriptions” Subjects and Themes:
- Subjects: Aircraft configurations - Computational geometry - Computational grids - Grid generation (Mathematics) - Surface geometry
Edition Identifiers:
- The Open Library ID: OL15400563M
Author's Alternative Names:
"Raymond L Barger"Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Automatic procedures for computing complete configuration geometry from individual component descriptions
By Raymond L. Barger
“Automatic procedures for computing complete configuration geometry from individual component descriptions” Metadata:
- Title: ➤ Automatic procedures for computing complete configuration geometry from individual component descriptions
- Author: Raymond L. Barger
- Number of Pages: Median: 11
- Publisher: Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va
“Automatic procedures for computing complete configuration geometry from individual component descriptions” Subjects and Themes:
- Subjects: Aircraft configurations - Surface geometry
Edition Identifiers:
- The Open Library ID: OL19752777M
Author's Alternative Names:
"Raymond L Barger"Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Fuselage design for a specified Mach-sliced area distribution
By Raymond L. Barger
“Fuselage design for a specified Mach-sliced area distribution” Metadata:
- Title: ➤ Fuselage design for a specified Mach-sliced area distribution
- Author: Raymond L. Barger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Fuselage design for a specified Mach-sliced area distribution” Subjects and Themes:
- Subjects: Fuselages - Aircraft design - Aircraft configurations - Mach number - Noise reduction
Edition Identifiers:
- The Open Library ID: OL16135462M
Author's Alternative Names:
"Raymond L Barger"Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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34Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel
By Sharon S. Graves
“Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel” Metadata:
- Title: ➤ Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel
- Author: Sharon S. Graves
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel” Subjects and Themes:
- Subjects: ➤ Subsonic wind tunnels - Ground effect (Aerodynamics) - Aircraft configurations - Data acquisition - Aerodynamic forces - Aerodynamic configurations - Aircraft design - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17136813M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls
By Johannes M van Aken
“Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls” Metadata:
- Title: ➤ Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls
- Author: Johannes M van Aken
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Helicopter Society - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - [Washington, DC - [Alexandria, Va.]
“Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls” Subjects and Themes:
- Subjects: ➤ Subsonic flutter - Joined wings - Structural stability - Aircraft configurations - Dynamic structural analysis - Aeroelasticity - Tilt rotor aircraft - Active control
Edition Identifiers:
- The Open Library ID: OL17000079M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36High speed research system study
By Jay R. Swink
“High speed research system study” Metadata:
- Title: ➤ High speed research system study
- Author: Jay R. Swink
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“High speed research system study” Subjects and Themes:
- Subjects: ➤ Aircraft configurations - Aircraft control - Aircraft design - Aircraft guidance - Cockpits - High speed - In-flight monitoring - Noses (forebodies)
Edition Identifiers:
- The Open Library ID: OL16123788M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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37Numerical study of steady and unsteady canard-wing-body aerodynamics
By Eugene L. Tu
“Numerical study of steady and unsteady canard-wing-body aerodynamics” Metadata:
- Title: ➤ Numerical study of steady and unsteady canard-wing-body aerodynamics
- Author: Eugene L. Tu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Numerical study of steady and unsteady canard-wing-body aerodynamics” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Unsteady aerodynamics - Canard configurations - Aircraft configurations - Aerodynamic characteristics - Control surfaces - Aerodynamic configurations - Flow distribution - Wings
Edition Identifiers:
- The Open Library ID: OL15498139M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration
By Angelen Ngan
“Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration” Metadata:
- Title: ➤ Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration
- Author: Angelen Ngan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration” Subjects and Themes:
- Subjects: ➤ Fighter aircraft - Structural analysis - Aircraft design - Aircraft configurations - Applications programs (Computers) - Design analysis
Edition Identifiers:
- The Open Library ID: OL15499055M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Preliminary design and analysis of procedures for the numerical generation of 3D block-structured grids
By J. W. Boerstoel
“Preliminary design and analysis of procedures for the numerical generation of 3D block-structured grids” Metadata:
- Title: ➤ Preliminary design and analysis of procedures for the numerical generation of 3D block-structured grids
- Author: J. W. Boerstoel
- Number of Pages: Median: 78
- Publisher: National Aerospace Laboratory
- Publish Date: 1986
- Publish Location: Amsterdam
“Preliminary design and analysis of procedures for the numerical generation of 3D block-structured grids” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19253093M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Variable-complexity multidisciplinary optimization on parallel computers
By Bernard Grossman
“Variable-complexity multidisciplinary optimization on parallel computers” Metadata:
- Title: ➤ Variable-complexity multidisciplinary optimization on parallel computers
- Author: Bernard Grossman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MAD Center, Virginia Polytechnic Institute and State University
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC - Blacksburg, Va
“Variable-complexity multidisciplinary optimization on parallel computers” Subjects and Themes:
- Subjects: ➤ Parallel computers - Multidisciplinary design optimization - Finite element method - Supercomputers - Aircraft configurations - Parallel processing (Computers) - Design analysis
Edition Identifiers:
- The Open Library ID: OL17582060M
- Online Computer Library Center (OCLC) ID: 41340751
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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