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Source: The Open Library
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Search results from The Open Library
1An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients
By Leland A. Carlson
“An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients” Metadata:
- Title: ➤ An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients
- Author: Leland A. Carlson
- Language: English
- Publisher: ➤ Aerospace Engineering Dept., Texas A&M University, Texas Engineering Experiment Station - National Aeronautics and Space Administration - National Technical Information Service, distributor - Aerospace Engineering Dept., Texas A&M University - National Aeronautics and Space Administration]
- Publish Date: 1988 - 1991 - 1992 - 1994
- Publish Location: ➤ College Station, Tex - Springfield, Va - [Washington, D.C
“An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aerodynamics - Aerodynamics, Transonic - Boundary value problems - Computational fluid dynamics - Finite difference theory - Influence coefficient - Mathematical models - Perturbation theory - Problem solving - Sensitivity - Three dimensional flow - Transonic Aerodynamics - Transonic flow - Wings
Edition Identifiers:
- The Open Library ID: ➤ OL15368439M - OL16123952M - OL15286296M - OL17633074M - OL17681999M - OL14707568M - OL15447192M - OL17679974M
- Online Computer Library Center (OCLC) ID: 58990739
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2High-lift systems on commercial subsonic airliners
By Peter K. C. Rudolph
“High-lift systems on commercial subsonic airliners” Metadata:
- Title: ➤ High-lift systems on commercial subsonic airliners
- Author: Peter K. C. Rudolph
- Language: English
- Number of Pages: Median: 155
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“High-lift systems on commercial subsonic airliners” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aeronautics, Commercial - Airplanes - Attitude (Inclination) - Commercial Aeronautics - Commercial aircraft - Cost analysis - Design analysis - Design and construction - Leading edge flaps - Leading edges - Lift (Aerodynamics) - Lift devices - Trailing edge flaps - Trailing edges - Wing camber - Wing loading - Wing slots
Edition Identifiers:
- The Open Library ID: OL15504955M - OL17576368M - OL18121439M - OL17125763M - OL19287956M
- Online Computer Library Center (OCLC) ID: 39916172
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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3Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
By David E. Hahne
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:
- Title: ➤ Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Springfield, VA - Hampton, Va
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Aerodynamic stability - Aerodynamics, Hypersonic - Angle of attack - Hypersonic Aerodynamics - Hypersonic speed - Hypersonic vehicles - Low speed - Mach number - Pitching moments - Stability - Stability of airplanes - Stabilizers (Fluid dynamics) - Vortices - Waveriders - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL18134999M - OL17133262M - OL17839424M - OL21033491M - OL15549003M
- Online Computer Library Center (OCLC) ID: 42055832
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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42-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:
- Title: ➤ 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- Author: R. A. Piziali
- Language: English
- Number of Pages: Median: 559
- Publisher: ➤ National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic coefficients - Pressure distribution - Wind tunnel tests - Wind oscillations - Angle of attack - Airfoils - Aerodynamic stalling - Semispan models - Stalling - Oscillating wing aerodynamics
Edition Identifiers:
- The Open Library ID: OL17007551M - OL15409387M - OL18079048M - OL19754822M - OL17114716M
- Online Computer Library Center (OCLC) ID: 32770651
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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5Two-dimensional high-lift aerodynamic optimization using neural networks
By Roxana M. Greenman
“Two-dimensional high-lift aerodynamic optimization using neural networks” Metadata:
- Title: ➤ Two-dimensional high-lift aerodynamic optimization using neural networks
- Author: Roxana M. Greenman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Moffett Field, Calif
“Two-dimensional high-lift aerodynamic optimization using neural networks” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computers - Navier-Stokes equation - Lift - Neural nets - Airfoils - Aerodynamic configurations - Angle of attack - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL17129961M - OL17580142M - OL18132744M - OL15542052M
- Online Computer Library Center (OCLC) ID: 41151565
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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6IPAC--Inlet Performance Analysis Code
By Paul J. Barnhart
“IPAC--Inlet Performance Analysis Code” Metadata:
- Title: ➤ IPAC--Inlet Performance Analysis Code
- Author: Paul J. Barnhart
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“IPAC--Inlet Performance Analysis Code” Subjects and Themes:
- Subjects: ➤ Engine inlets - Inlet flow - Aerodynamic coefficients - Pressure recovery - Aerodynamic drag - Reliability analysis
Edition Identifiers:
- The Open Library ID: OL18115388M - OL17564997M - OL17123843M - OL15489478M
- Online Computer Library Center (OCLC) ID: 39289699
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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7Hypersonic pitching-moment shift for stardust reentry capsule forebody
By William A. Wood
“Hypersonic pitching-moment shift for stardust reentry capsule forebody” Metadata:
- Title: ➤ Hypersonic pitching-moment shift for stardust reentry capsule forebody
- Author: William A. Wood
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Hypersonic pitching-moment shift for stardust reentry capsule forebody” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computational fluid dynamics - Hypersonic flow - Mach number - Navier-Stokes equation - Pitching moments - Space capsules
Edition Identifiers:
- The Open Library ID: OL17582192M - OL18137055M - OL15554563M - OL17132065M
- Online Computer Library Center (OCLC) ID: 41618396
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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8Determining the accuracy of aerodynamic model parameters estimated from flight test data
By Eugene A. Morelli
“Determining the accuracy of aerodynamic model parameters estimated from flight test data” Metadata:
- Title: ➤ Determining the accuracy of aerodynamic model parameters estimated from flight test data
- Author: Eugene A. Morelli
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Determining the accuracy of aerodynamic model parameters estimated from flight test data” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Aerodynamic coefficients - Maximum likelihood estimates - Monte Carlo method - Research vehicles
Edition Identifiers:
- The Open Library ID: OL17122769M - OL17695368M - OL17827039M
- Online Computer Library Center (OCLC) ID: 38860609
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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9Application of two procedures for dual-point design of transonic airfoils
By Raymond E. Mineck
“Application of two procedures for dual-point design of transonic airfoils” Metadata:
- Title: ➤ Application of two procedures for dual-point design of transonic airfoils
- Author: Raymond E. Mineck
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Application of two procedures for dual-point design of transonic airfoils” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aircraft landing - F-15 aircraft - Flight control - Flight tests - Ground effect (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15403118M - OL19917053M - OL17788397M
- Online Computer Library Center (OCLC) ID: 32185117
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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10Flight-measured laminar boundary-layer transition phenomena including stability theory analysis
By Clifford J. Obara
“Flight-measured laminar boundary-layer transition phenomena including stability theory analysis” Metadata:
- Title: ➤ Flight-measured laminar boundary-layer transition phenomena including stability theory analysis
- Author: Clifford J. Obara
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service,] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Flight-measured laminar boundary-layer transition phenomena including stability theory analysis” Subjects and Themes:
- Subjects: ➤ Laminar flow - Turbulent boundary layer - Aerodynamic coefficients - Boundary layer transition - Boundary layer - Transition flow
Edition Identifiers:
- The Open Library ID: OL16115008M - OL18217710M - OL18468555M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data
By Michael D. Messina
“Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data” Metadata:
- Title: ➤ Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data
- Author: Michael D. Messina
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Flight simulation - Flight tests - Forebodies - Strakes - Yawing moments
Edition Identifiers:
- The Open Library ID: OL15423138M - OL17796495M
- Online Computer Library Center (OCLC) ID: 35248154
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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12Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
By Jensen Lin
“Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation” Metadata:
- Title: ➤ Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Author: Jensen Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aeroelasticity - Laplace transformation - Lift - Method of moments - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17596830M - OL17704161M
- Online Computer Library Center (OCLC) ID: 45009645
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
By Dale Ashby
“Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Metadata:
- Title: ➤ Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- Author: Dale Ashby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Stanford, Calif.] - [Washington, DC - Springfield, Va
“Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Airfoils - Boundary layer separation - Flaps (Control surfaces) - Incompressible flow - Lift augmentation - Potential flow - Pressure distribution - Separated flow - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL15505042M - OL17838000M
- Online Computer Library Center (OCLC) ID: 40101894
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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14Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
By Jim A. Penland
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:
- Title: ➤ Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Author: Jim A. Penland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent boundary layer - Aerodynamic coefficients - Body-wing configurations - Reynolds number - Hypersonic forces - Hypersonic boundary layer - Aerodynamic drag - Hypersonic shock - Mach number
Edition Identifiers:
- The Open Library ID: OL17591848M - OL15548849M
- Online Computer Library Center (OCLC) ID: 42677545
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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15Modeling the high speed research cycle 2B longitudinal aerodynamic database using nultivariate orthogonal functions
By E. A. Morelli
“Modeling the high speed research cycle 2B longitudinal aerodynamic database using nultivariate orthogonal functions” Metadata:
- Title: ➤ Modeling the high speed research cycle 2B longitudinal aerodynamic database using nultivariate orthogonal functions
- Author: E. A. Morelli
- 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
“Modeling the high speed research cycle 2B longitudinal aerodynamic database using nultivariate orthogonal functions” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Civil aviation - High speed - Models - Orthogonal Functions - Polynomials - Tabulation processes - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15567869M - OL17595196M
- Online Computer Library Center (OCLC) ID: 44187622
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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16Turbulence measurements on a flap-edge model
By Patrick Moriarty
“Turbulence measurements on a flap-edge model” Metadata:
- Title: ➤ Turbulence measurements on a flap-edge model
- Author: Patrick Moriarty
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Turbulence measurements on a flap-edge model” Subjects and Themes:
- Subjects: ➤ Velocity measurement - Wire - Flow measurement - Turbulence - Aerodynamic coefficients - Pressure sensors
Edition Identifiers:
- The Open Library ID: OL17839110M
- Online Computer Library Center (OCLC) ID: 41378463
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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17Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
By Kevin W. Noonan
“Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade” Metadata:
- Title: ➤ Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
- Author: Kevin W. Noonan
- Language: English
- Number of Pages: Median: 86
- 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, D.C
“Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade” Subjects and Themes:
- Subjects: ➤ Statistics - Aerodynamic coefficients - Aerodynamics - Testing - Aerodynamic characteristics - Rotary wing aircraft - Rotary wings - Aerofoils - Rotors (Helicopters)
Edition Identifiers:
- The Open Library ID: OL18246790M
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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18Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1
By A. M. Morrison
“Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1” Metadata:
- Title: ➤ Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1
- Author: A. M. Morrison
- Number of Pages: Median: 554
- Publisher: Naval Surface Weapons Center
- Publish Date: 1975
- Publish Location: Silver Spring, Md
“Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19047093M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Experimental optimization methods for multi-element airfoils
By Drew Landman
“Experimental optimization methods for multi-element airfoils” Metadata:
- Title: ➤ Experimental optimization methods for multi-element airfoils
- Author: Drew Landman
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Norfolk, Va - [Washington, DC - Springfield, Va
“Experimental optimization methods for multi-element airfoils” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Reynolds number - Angle of attack - Pressure distribution - Flaps (Control surfaces) - Optimization - Airfoils - Computer programs
Edition Identifiers:
- The Open Library ID: OL15506398M
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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20Aeroelastic calculations using CFD for a typical business jet model
By Michael D. Gibbons
“Aeroelastic calculations using CFD for a typical business jet model” Metadata:
- Title: ➤ Aeroelastic calculations using CFD for a typical business jet model
- Author: Michael D. Gibbons
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1996
- Publish Location: Springfield, VA - Hampton, Va
“Aeroelastic calculations using CFD for a typical business jet model” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Viscous flow - Flexible wings - Navier-Stokes equation - Aerodynamic coefficients - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL15490455M
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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21An aerodynamic tradeoff study of the scissor wing configuration
By Bruce P. Selberg
“An aerodynamic tradeoff study of the scissor wing configuration” Metadata:
- Title: ➤ An aerodynamic tradeoff study of the scissor wing configuration
- Author: Bruce P. Selberg
- Language: English
- Publisher: ➤ University of Missouri-Rolla - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Hampton, Va - Rolla, Mo
“An aerodynamic tradeoff study of the scissor wing configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Lift drag ratio - Design and construction - Aircraft stability - Supersonic flight - Aerofoils - Aerodynamic configurations - Variable sweep wings
Edition Identifiers:
- The Open Library ID: OL16128718M
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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22Design and performance calculations of a propeller for very high altitude flight
By L. Danielle Koch
“Design and performance calculations of a propeller for very high altitude flight” Metadata:
- Title: ➤ Design and performance calculations of a propeller for very high altitude flight
- Author: L. Danielle Koch
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Design and performance calculations of a propeller for very high altitude flight” Subjects and Themes:
- Subjects: ➤ Prop-fan technology - Numerical analysis - Aerodynamic coefficients - Propellers - Navier-Stokes equation - Performance prediction - Propeller efficiency - Angle of attack - Low Reynolds number
Edition Identifiers:
- The Open Library ID: OL15543200M
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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23Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
By William B. Compton
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Metadata:
- Title: ➤ Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Author: William B. Compton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Angle of attack - Axisymmetric flow - Computational fluid dynamics - Convergent-divergent nozzles - Exhaust gases - Free flow - Jet exhaust - K-epsilon turbulence model - Navier-Stokes equation - Nozzle flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15504433M
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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24User's manual for FOMOCO utilities-force and moment computation tools for overset grids
By William M. Chan
“User's manual for FOMOCO utilities-force and moment computation tools for overset grids” Metadata:
- Title: ➤ User's manual for FOMOCO utilities-force and moment computation tools for overset grids
- Author: William M. Chan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“User's manual for FOMOCO utilities-force and moment computation tools for overset grids” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Mass flow rate - Aerodynamic coefficients - Computational grids - User manuals (Computer programs) - Grid generation (Mathematics) - Applications programs (Computers)
Edition Identifiers:
- The Open Library ID: OL15498149M
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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25Modern airfoil ice accretions
By Harold E. Addy
“Modern airfoil ice accretions” Metadata:
- Title: Modern airfoil ice accretions
- Author: Harold E. Addy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Washington, DC
“Modern airfoil ice accretions” Subjects and Themes:
- Subjects: Ice formation - Aerodynamic characteristics - Aerodynamic coefficients - Airfoils - Computer programs
Edition Identifiers:
- The Open Library ID: OL17120505M
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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26Comparison of several dissipation algorithms for central difference schemes
By R. Charles Swanson
“Comparison of several dissipation algorithms for central difference schemes” Metadata:
- Title: ➤ Comparison of several dissipation algorithms for central difference schemes
- Author: R. Charles Swanson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, VA
“Comparison of several dissipation algorithms for central difference schemes” Subjects and Themes:
- Subjects: ➤ Differential equations - Flow equations - Aerodynamic coefficients - Finite volume method - Navier-Stokes equation - Airfoils - Internal waves - Shock waves
Edition Identifiers:
- The Open Library ID: OL15505149M
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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27Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
By Ramadas K. Prabhu
“Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees” Metadata:
- Title: ➤ Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Aerodynamic coefficients - Space shuttle orbiters - Angle of attack - Hypersonic speed - Aerodynamic characteristics - Mach number
Edition Identifiers:
- The Open Library ID: OL16042466M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
By Margaret Anne Menzies
“Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Metadata:
- Title: ➤ Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
- Author: Margaret Anne Menzies
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Old Dominion University - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Norfolk, VA - Washington, D.C
“Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Subjects and Themes:
- Subjects: ➤ Flow equations - Aerodynamic coefficients - Unsteady flow - Transonic flow - Swept wings - Navier-Stokes equation - Angle of attack - Delta wings - Leading edges - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15508551M
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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29Study of the TRAC airfoil table computational system
By Hong Hu
“Study of the TRAC airfoil table computational system” Metadata:
- Title: ➤ Study of the TRAC airfoil table computational system
- Author: Hong Hu
- 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
“Study of the TRAC airfoil table computational system” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aerodynamic coefficients - Navier-Stokes equation - Pitching moments - Drag - Lift - Airfoils - Noise reduction - Computer programs - Aerodynamic noise
Edition Identifiers:
- The Open Library ID: OL15550693M
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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30Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
By E. Carson Yates
“Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory” Metadata:
- Title: ➤ Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
- Author: E. Carson Yates
- Language: English
- Number of Pages: Median: 16
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory” Subjects and Themes:
- Subjects: ➤ Surfaces - Lift - Aerodynamic coefficients - Unsteady flow - Aerodynamics - Sensitivity - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15409051M
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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31Venusian atmospheric and Magellan properties from attitude cotrol data
By Christopher A. Croom
“Venusian atmospheric and Magellan properties from attitude cotrol data” Metadata:
- Title: ➤ Venusian atmospheric and Magellan properties from attitude cotrol data
- Author: Christopher A. Croom
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Venusian atmospheric and Magellan properties from attitude cotrol data” Subjects and Themes:
- Subjects: ➤ Moment distribution - Aerodynamic coefficients - Attitude control - Venus atmosphere - Stability derivatives - Magellan spacecraft (NASA)
Edition Identifiers:
- The Open Library ID: OL15404043M
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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32A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
By Bandu N. Pamadi
“A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept” Metadata:
- Title: ➤ A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
- Author: Bandu N. Pamadi
- 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
“A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Mathematical models - Angle of attack - Pitching moments - Lift - Aerodynamic drag - Hypersonic aircraft - Aerospace planes - Mach number
Edition Identifiers:
- The Open Library ID: OL15403126M
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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33Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
By Steven M. Klausmeyer
“Comparative results from a CFD challenge over a 2D three-element high-lift airfoil” Metadata:
- Title: ➤ Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Author: Steven M. Klausmeyer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Comparative results from a CFD challenge over a 2D three-element high-lift airfoil” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Aerodynamic coefficients - Lift - Airfoils - Navier-Stokes equation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15497745M
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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34An approach to the constrained design of natural laminar flow airfoils
By Bradford Earl Green
“An approach to the constrained design of natural laminar flow airfoils” Metadata:
- Title: ➤ An approach to the constrained design of natural laminar flow airfoils
- Author: Bradford Earl Green
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“An approach to the constrained design of natural laminar flow airfoils” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Turbulent boundary layer - Lift - Aerodynamic coefficients - Laminar flow airfoils - Laminar boundary layer - Pressure distribution
Edition Identifiers:
- The Open Library ID: OL15498378M
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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35Sensitivity analysis for coupled aero-structural systems
By Anthony A. Giunta
“Sensitivity analysis for coupled aero-structural systems” Metadata:
- Title: ➤ Sensitivity analysis for coupled aero-structural systems
- Author: Anthony A. Giunta
- 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
“Sensitivity analysis for coupled aero-structural systems” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aerodynamic forces - Sensitivity - Aircraft design - Structural analysis - Design analysis
Edition Identifiers:
- The Open Library ID: OL15557238M
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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36Development of multiobjective optimization techniques for sonic boom minimization
By Aditi Chattopadhyay
“Development of multiobjective optimization techniques for sonic boom minimization” Metadata:
- Title: ➤ Development of multiobjective optimization techniques for sonic boom minimization
- Author: Aditi Chattopadhyay
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Development of multiobjective optimization techniques for sonic boom minimization” Subjects and Themes:
- Subjects: ➤ Optimization - Aerodynamic coefficients - Sonic booms - Aerodynamics - Overpressure - Aerospace vehicles - Life drag ratio
Edition Identifiers:
- The Open Library ID: OL15419648M
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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