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1
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84894366233
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Helicopter Free Wake Predictions of Complex Wake Structures Under Blade-Vortex Interaction Operating Conditions
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Presented at, June 16-18
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Egolf, T. A., "Helicopter Free Wake Predictions of Complex Wake Structures Under Blade-Vortex Interaction Operating Conditions", Presented at 44th Annual Forum and Technology Display of the American Helicopter Society, June 16-18, 1988.
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(1988)
44th Annual Forum and Technology Display of the American Helicopter Society
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Egolf, T.A.1
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3
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0029344786
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Rotor Free-Wake Modeling using a Pseudo-Implicit Technique-Including Comparisons with Experiment
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July
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Bagai, A., and Leishman, J. G., "Rotor Free-Wake Modeling using a Pseudo-Implicit Technique-Including Comparisons with Experiment, " Journal of the American Helicopter Society, Vol. 40, No. 3, July 1995, pp. 29-41.
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Journal of the American Helicopter Society
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, Issue.3
, pp. 29-41
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Bagai, A.1
Leishman, J.G.2
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5
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0014590930
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An Analytical Method for Predicting Rotor Wake Geometry
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October
-
Landgrebe, A. J., "An Analytical Method for Predicting Rotor Wake Geometry", Journal Of the American Helicopter Society, Vol. 14, No. 4, October 1969.
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(1969)
Journal Of the American Helicopter Society
, vol.14
, Issue.4
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Landgrebe, A.J.1
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6
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0003995112
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NASA CR 3726, October
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Egolf, T. A. and A.J. Landgrebe, "Helicopter Rotor Wake Geometry And Its Influence In Forward Flight, Volume I-Generalized Wake Geometry and Wake Effect on Rotor Airloads and Performance", NASA CR 3726, October, 1983.
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(1983)
Helicopter Rotor Wake Geometry And Its Influence In Forward Flight, Volume I-Generalized Wake Geometry and Wake Effect on Rotor Airloads and Performance
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Egolf, T.A.1
Landgrebe, A.J.2
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7
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84894378338
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NASA CR 194894, May
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Quackenbush, T. R., C.-M. Gordon Lam, and D. A. Wachpress, Computational Analysis of High Resolution Unsteady Airloads for Rotor Aeroacoustics, NASA CR 194894, May 1994.
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(1994)
Computational Analysis of High Resolution Unsteady Airloads for Rotor Aeroacoustics
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Quackenbush, T.R.1
Gordon Lam, C.-M.2
Wachpress, D.A.3
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8
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84894346684
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A Multi-Element Vortex Lattice Method for Calculating the Geometry and effects of a Helicopter Rotor wake in Forward Flight
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AIAA-88-0664, Reno NV, January
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Berry, J. D., "A Multi-Element Vortex Lattice Method for Calculating the Geometry and effects of a Helicopter Rotor wake in Forward Flight", AIAA 26th Aerospace Sciences meeting, AIAA-88-0664, Reno NV, January 1988.
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(1988)
AIAA 26th Aerospace Sciences meeting
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-
Berry, J.D.1
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9
-
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0342398420
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Helicopter Free Wake Implementation On Advanced Computer Architectures
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Presented at The, University of Maryland, College Park, Maryland, February 16-18
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Egolf, T. A., and J.P. Massar, "Helicopter Free Wake Implementation On Advanced Computer Architectures", Presented at The 2nd International Conference on Basic Rotorcraft Research, University of Maryland, College Park, Maryland, February 16-18, 1988.
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(1988)
2nd International Conference on Basic Rotorcraft Research
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Egolf, T.A.1
Massar, J.P.2
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10
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0022463804
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Time-History Analysis for Rotorcraft Dynamics based on a Component Approach'
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January
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Sopher, R., and Hallock, D. W., "Time-History Analysis for Rotorcraft Dynamics based on a Component Approach'", Journal of the American Helicopter Society, Vol. 31, 91), January 1986.
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(1986)
Journal of the American Helicopter Society
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, Issue.91
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Sopher, R.1
Hallock, D.W.2
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14
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0016529838
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Estimation of Velocities and Roll-Up in Aircraft Vortex Wakes
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July
-
Bilanin, A. J. and Donaldson, C. duP., "Estimation of Velocities and Roll-Up in Aircraft Vortex Wakes, " Journal of Aircraft, Vol. 12, No. 7, July 1975.
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(1975)
Journal of Aircraft
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Bilanin, A.J.1
Donaldson, C.2
du, P.3
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16
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0016383509
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A Numerical Study of the Rollup of a Finite Vortex Sheet
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Moore, D. W., "A Numerical Study of the Rollup of a Finite Vortex Sheet, " Journal of Fluid Mechanics, Vol. 63, Part 2, pp. 225-235, 1974.
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Journal of Fluid Mechanics
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, pp. 225-235
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Moore, D.W.1
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17
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2942591743
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-
IB 129-95/28, Dec
-
Splettstoesser, W.R., Kube, R., Seelhorst, U., Wagner, W., et. al., "Higher Harmonic Control Aeroacoustic Rotor Test (HART)-Test Documentation and Representative Results, " IB 129-95/28, Dec. 1995.
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(1995)
Higher Harmonic Control Aeroacoustic Rotor Test (HART)-Test Documentation and Representative Results
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Splettstoesser, W.R.1
Kube, R.2
Seelhorst, U.3
Wagner, W.4
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19
-
-
0033115812
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An Overset Grid Navier-Stokes Kirchhoff-Surface Method for Rotorcraft Aero-Acoustics Predictions
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Strawn, R.C., Duque, E.P. N, and Ahmad, J., "An Overset Grid Navier-Stokes Kirchhoff-Surface Method for Rotorcraft Aero-Acoustics Predictions, " AHS Journal, 44, 132-140, 1999.
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AHS Journal
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Strawn, R.C.1
Duque, E.P.N.2
Ahmad, J.3
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24
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84894369691
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Investigation of High-Order Upwinded Differencing for Vortex Convection
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Sept
-
Wake, B. E. and D. Choi, "Investigation of High-Order Upwinded Differencing for Vortex Convection, " UTRC Memorandum, Sept. 1994.
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(1994)
UTRC Memorandum
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Wake, B.E.1
Choi, D.2
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25
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0029673397
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Investigation of Higher-Order Upwinded Differencing for Vortex Convection
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Wake, B.E. and D. Choi, "Investigation of Higher-Order Upwinded Differencing for Vortex Convection, AIAA Journal, Vol. 34, pp332-337, 1995.
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AIAA Journal
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Wake, B.E.1
Choi, D.2
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26
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33746600503
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Resolution and Convection of Tip Vortex Using Higher-Order Methods
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Accepted for publication
-
Wake, B.E., T. A. Egolf, and D. Choi, "Resolution and Convection of Tip Vortex Using Higher-Order Methods, " Journal of Computational Physics, Accepted for publication.
-
Journal of Computational Physics
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Wake, B.E.1
Egolf, T.A.2
Choi, D.3
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29
-
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84894382162
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Implementation of High-Order Differencing into CFL3D for Vortex Resolutions
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Dec. 22
-
Wake, B.E., Egolf, T.A., and Choi, D., "Implementation of High-Order Differencing into CFL3D for Vortex Resolutions, " UTRC Memorandum, Dec. 22, 1995.
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(1995)
UTRC Memorandum
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Wake, B.E.1
Egolf, T.A.2
Choi, D.3
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30
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78149435357
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Numerical Simulation of the Space Shuttle Launch Vehicle Flowfield with Real Gas Solid Rocket Motor Plume Effects
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AIAA-93-0521, Reno, NV, January 11-14
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Slotnick, J. P., Kandula, M., Buning P.G., and Martin, F.W. Jr., "Numerical Simulation of the Space Shuttle Launch Vehicle Flowfield with Real Gas Solid Rocket Motor Plume Effects, " AIAA-93-0521, 31st Aerospace Sciences Meeting & Exhibit, Reno, NV, January 11-14, 1993.
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(1993)
31st Aerospace Sciences Meeting & Exhibit
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Slotnick, J.P.1
Kandula, M.2
Buning, P.G.3
Martin Jr., F.W.4
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31
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84997605024
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Implementation of LU-SGS Algorithm and Roe Upwinding scheme in OVERFLOW Thin-Layer Navier Stokes Code
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AIAA-942357, Colorado Springs, CO, June 20-23
-
Kandula, M. and Buning, P.G., "Implementation of LU-SGS Algorithm and Roe Upwinding scheme in OVERFLOW Thin-Layer Navier Stokes Code, "AIAA-942357, 25th AIAA Fluid Dynamics Conference, Colorado Springs, CO, June 20-23, 1994.
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(1994)
25th AIAA Fluid Dynamics Conference
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Kandula, M.1
Buning, P.G.2
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32
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0029708250
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Helicopter Rotor Blade Computation in Unsteady Flows Using Moving Overset Grids
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Jan.-Feb
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Ahmad, J. And Duque, E. P. N., "Helicopter Rotor Blade Computation in Unsteady Flows Using Moving Overset Grids, " Journal Of Aircraft Vol. 33, No. 1, pp 54-60, Jan.-Feb. 1996.
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Journal Of Aircraft
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Ahmad, J.1
Duque, E.P.N.2
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33
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84894304831
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UTRC Report No. R96-5.200.0005, Contract NAS2-14094, Nov
-
Egolf, T. A. and B. E. Wake, "Development and Application of a Numerical Rotorcraft Test facility for Tilt-Rotor Interactional Aerodynamics, Phase 1-Initial Infrastructure Development and Assessment, " UTRC Report No. R96-5.200.0005, Contract NAS2-14094, Nov. 1996
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Development and Application of a Numerical Rotorcraft Test facility for Tilt-Rotor Interactional Aerodynamics, Phase 1-Initial Infrastructure Development and Assessment
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Egolf, T.A.1
Wake, B.E.2
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34
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0029760797
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Evaluation of a Navier-Stokes Analysis for Hover Performance Prediction
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Jan
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Wake, B.E., and Baeder, J.D., "Evaluation of a Navier-Stokes Analysis for Hover Performance Prediction, " Journal of the American Helicopter Society, Vol. 41, No. 1, Jan 1996, pp. 7-17.
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Journal of the American Helicopter Society
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Wake, B.E.1
Baeder, J.D.2
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