#
Aerodynamic coefficients
Resource Information
The concept ** Aerodynamic coefficients** represents the subject, aboutness, idea or notion of resources found in **University of Missouri-St. Louis Libraries**.

The Resource
Aerodynamic coefficients
Resource Information

The concept

**Aerodynamic coefficients**represents the subject, aboutness, idea or notion of resources found in**University of Missouri-St. Louis Libraries**.- Label
- Aerodynamic coefficients

- Source
- nasat

## Context

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- Validation of 3-D ice accretion measurement methodology for experimental aerodynamic simulation
- A non-cut cell immersed boundary method for use in icing simulations
- Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
- Aerodynamic coefficients from aeroballistic range testing of deployed-and stowed-SIAD SFDT models
- Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Aeroelastic calculations using CFD for a typical business jet model
- An aerodynamic analysis computer program and design notes for low speed wing flap systems
- An aerodynamic tradeoff study of the scissor wing configuration
- An analysis for high speed propeller-nacelle aerodynamic performance prediction
- An approach to the constrained design of natural laminar flow airfoils : a thesis ...
- An evaluation of performance metrics for high efficiency tube-and-wing aircraft entering service in 2030-2035
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, January 1991 - June 1991
- Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation
- Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove
- Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft
- Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft
- Application of approximate unsteady aerodynamics for flutter analysis
- Basis function approximation of transonic aerodynamic influence coefficient matrix
- Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method
- Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Comparison of several dissipation algorithms for central difference schemes
- Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Computer program for post-flight analysis of rigid body moments acting on a launch vehicle first stage
- Convergence analysis of turbulent flow solutions
- Design and performance calculations of a propeller for very high altitude flight
- Design of a slotted, natural-laminar-flow airfoil for a transport aircraft
- Determining the accuracy of aerodynamic model parameters estimated from flight test data
- Dynamic stability instrumentation system (DSIS)
- Estimates for the aerodynamic coefficients of ringsail and disk-gap-band parachutes operating on Mars
- Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- Experimental optimization methods for multi-element airfoils : final report
- Flight measurements of hinged-plate wing-spoiler hinge moments
- Flight-measured laminar boundary layer transition phenomena including stability theory analysis
- High-lift systems on commercial subsonic airliners
- Hypersonic pitching-moment shift for stardust reentry capsule forebody
- IPAC--Inlet Performance Analysis Code
- Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Modeling the high speed research cycle 2B longitudinal aerodynamic database using multivariate orthogonal functions
- Modern airfoil ice accretions
- Modern airfoil ice accretions
- Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20
- Potential benefits of magnetic suspension and balance systems
- Rarefaction effects on Galileo probe aerodynamics
- Rarefaction effects on Galileo probe aerodynamics
- Real-time method for estimating viscous forebody drag coefficients
- Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane
- Sensitivity analysis for coupled aero-structural systems
- Study of the TRAC airfoil table computational system
- Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data
- Theory of wing rock
- Turbulence measurements on a flap-edge model : final report : NASA-Ames university consortium, NCC2-5140
- Two-dimensional high-lift aerodynamic optimization using neural networks
- Unsteady aerodynamic model tuning for precise flutter prediction
- Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem
- User's manual for FOMOCO utilities : Force and Moment Computation tools for overset grids
- User's manual for FOMOCO utilities-force and moment computation tools for overset grids

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`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/2DhoSDZkMeI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/2DhoSDZkMeI/">Aerodynamic coefficients</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>`