Prediction of aircraft longitudinal response using time-accurate Euler computations

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 852-858

  Hulshoff, S J ^a   Hoeijmakers, H W M ^a   Mulder, J A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; VORTEX FLOW; WINGS;

AIRCRAFT DYNAMICS; EULER COMPUTATIONS; EULER SOLUTIONS; LONGITUDINAL RESPONSE; MULTI-GRID; TIME-ACCURATE;

AIRCRAFT;

EID: 84964204660     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2485     Document Type: Conference Paper

References (9)

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2. Hulshoff, S. J., “An Euler Solution Algorithm for Steady Helicopter-Rotor Flows” Ph. D. Thesis, Department of Aerospace Science and Engineering, University of Toronto, 1994.
3. Venkatakrishnan, V. and Jameson, A., “Computation of Unsteady Transonic Flows by the Solution of the Euler Equations, ” AIAA Journal, Vol. 26, No. 8, 1988.
4. Klopfer, G. H. and Molvik, G. A., “Conservative Mul-tizonal Interface Algorithm for the 3-D Navier-Stokes Equations, ” AIAA Paper No. 91-1601CP, June 1991.
5. Jameson, A., “Time Dependent Calculations Using Multigrid, with Applications to Unsteady Flows Past Airfoils and Wings, ” AIAA 91-1596, 10th Computational Fluid Dynamics Conference, June 24-26, 1991.
6. Lesieutre, D. J., Reisenthel, P. H., and Dillenius, M. F. E., “A Practical Approach for Calculating Aerodynamic Indicia1 Functions with a Navier-Stokes Solver” AIAA Paper No. 94-0059, 1994.
7. Schiff, L. B., and Katz, J. “Application of CFD Techniques Toward the Validation of Nonlinear Aerodynamic models, ” in “Unsteady Aerodynamics - Fundamentals and Applications to Aircraft Dynamics”, AGARD CP-386, 1985.
8. Tobak, M., and Schiff, L. B., “Aerodynamic Mathematical Modelling - Basic Concepts”, AGARD LS 114, Paper 1, March, 1981.
9. Bisplinghoff, R.L., Ashley, H., and Halfman, R.L. “Aeroelasticity” Addison-Wesley, Cambridge, Mass., 1955.