-
1
-
-
73349137744
-
Overview of circulation control pneumatic aerodynamics: Blown force and moment augmentation and modification as applied primarily to fixed-wing aircraft
-
NASA CP 2005-213509/PT1June
-
Englar, R. J., "Overview of Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modification as Applied Primarily to Fixed-Wing Aircraft," Proceedings of the 2004 NASA/ONR Circulation Control Workshop, NASA CP 2005-213509/PT1June 2005, pp. 37-100.
-
(2005)
Proceedings of the 2004 NASA/ONR Circulation Control Workshop
, pp. 37-100
-
-
Englar, R.J.1
-
2
-
-
25144520789
-
-
(January 1969 through December 1983)," David W. Taylor Naval Ship Research and Development Center DTNSRDC-84/052, Sept.
-
Englar, R. J., and Applegate, C. A., "Circulation Control: A Bibliography of DTNSRDC Research and Selected Outside References (January 1969 through December 1983)," David W. Taylor Naval Ship Research and Development Center DTNSRDC-84/052, Sept. 1984.
-
(1984)
Circulation Control: A Bibliography of DTNSRDC Research and Selected Outside References
-
-
Englar, R.J.1
Applegate, C.A.2
-
3
-
-
0344433293
-
Flight testing the circulation control wing
-
Aug.
-
Pugliese, A. J., and Englar, R. J., "Flight Testing the Circulation Control Wing," AIAA Paper 79-1791, Aug. 1979.
-
(1979)
AIAA Paper
, pp. 79-1791
-
-
Pugliese, A.J.1
Englar, R.J.2
-
4
-
-
79952805679
-
-
NASATM-84232, July
-
Eppel, J. G., Shovlin, M. D., Jaynes, D. N., Englar, R. J., and Nichols, J. H., Jr., "Static Investigation of the Circulation-Controlling/Upper- Surface Blowing Concept Applied to the Quiet Short-Haul Research Aircraft," NASATM-84232, July 1982.
-
(1982)
Static Investigation of the Circulation-Controlling/Upper- Surface Blowing Concept Applied to the Quiet Short-Haul Research Aircraft
-
-
Eppel, J.G.1
Shovlin, M.D.2
Jaynes, D.N.3
Englar, R.J.4
Nichols Jr., J.H.5
-
5
-
-
77953739469
-
-
M.S. Thesis, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, MD, June
-
Englar, R. J., "Experimental Investigation of the High Velocity Coanda Wall Jet Applied to Bluff Trailing Edge Circulation Control Airfoils," M.S. Thesis, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, MD, June 1973.
-
(1973)
Experimental Investigation of the High Velocity Coanda Wall Jet Applied to Bluff Trailing Edge Circulation Control Airfoils
-
-
Englar, R.J.1
-
6
-
-
33845253591
-
-
AIAA Paper 2006-3009, Jan.
-
Jones, G. S., Yao, C. S., and Allan, B. G., "Experimental Investigation of a 2D Supercritical Circulation-Control Airfoil Using Particle Image Velocimetry," AIAA Paper 2006-3009, Jan. 2006.
-
(2006)
Experimental Investigation of a 2D Supercritical Circulation-control Airfoil Using Particle Image Velocimetry
-
-
Jones, G.S.1
Yao, C.S.2
Allan, B.G.3
-
7
-
-
62249179354
-
-
AIAA, Reston, VA, June
-
Joslin, R., and Jones, G., Applications of Circulation Control Technology, Progress in Astronautics and Aeronautics, Vol. 214, AIAA, Reston, VA, June 2006.
-
(2006)
Applications of Circulation Control Technology, Progress in Astronautics and Aeronautics
, vol.214
-
-
Joslin, R.1
Jones, G.2
-
8
-
-
0028498946
-
Application of circulation control to advanced subsonic transport aircraft, Part I: Airfoil development
-
Sept. doi:10.2514/3.56907
-
Englar, R. J., Smith, M. J., Kelley, S. M., and Rover, R. C., III, "Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I: Airfoil Development," Journal of Aircraft, Vol. 31, No. 5, Sept. 1994, pp. 1160-1168. doi:10.2514/3.56907
-
(1994)
Journal of Aircraft
, vol.31
, Issue.5
, pp. 1160-1168
-
-
Englar, R.J.1
Smith, M.J.2
Kelley, S.M.3
Rover Iii, R.C.4
-
9
-
-
0028499645
-
Application of circulation control to advanced subsonic transport aircraft, Part II: Transport application
-
Sept. doi:10.2514/3.46627
-
Englar, R. J., Smith, M. J., Kelley, S. M., and Rover, R. C., III, "Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part II: Transport Application," Journal of Aircraft, Vol. 31, No. 5, Sept. 1994, pp. 1169-1177. doi:10.2514/3.46627
-
(1994)
Journal of Aircraft
, vol.31
, Issue.5
, pp. 1169-1177
-
-
Englar, R.J.1
Smith, M.J.2
Kelley, S.M.3
Rover Iii, R.C.4
-
10
-
-
2942753911
-
-
AIAA Paper 2004-0056, Jan.
-
Liu, Y., Sankar, L. N., Englar, R. J., Ahuja, K., and Gaeta, R., "Computational Evaluation of the Steady and Pulsed Jet Effects on the Performance of a Circulation Control Wing Section," AIAA Paper 2004-0056, Jan. 2004.
-
(2004)
Computational Evaluation of the Steady and Pulsed Jet Effects on the Performance of a Circulation Control Wing Section
-
-
Liu, Y.1
Sankar, L.N.2
Englar, R.J.3
Ahuja, K.4
Gaeta, R.5
-
13
-
-
0002054570
-
Comments on the feasibility of les for wings and on a hybrid RANS/LES approach
-
Greyden Press, Columbus, OH
-
Spalart, P. R., Jou, W.-H., Strelets, M., and Allmaras, S., "Comments on the Feasibility of LES for Wings and on a Hybrid RANS/LES Approach," Proceedings of the 1st AFOSR International Conference on DNS/LES, Greyden Press, Columbus, OH, 1997, pp. 137-147.
-
(1997)
Proceedings of the 1st AFOSR International Conference on DNS/LES
, pp. 137-147
-
-
Spalart, P.R.1
Jou, W.-H.2
Strelets, M.3
Allmaras, S.4
-
14
-
-
0028486598
-
Two-equation eddy-viscosity turbulence models for engineering applications
-
Aug. doi:10.2514/3.12149
-
Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, Aug. 1994, pp. 1598-1605. doi:10.2514/3.12149
-
(1994)
AIAA Journal
, vol.32
, Issue.8
, pp. 1598-1605
-
-
Menter, F.R.1
-
15
-
-
0000034725
-
Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws
-
edited by A. Quarteroni, Lecture Notes in Mathematics, Springer, New York
-
Shu, C. W., "Essentially Non-Oscillatory and Weighted Essentially Non-Oscillatory Schemes for Hyperbolic Conservation Laws," Advanced Numerical Approximation of Nonlinear Hyperbolic Equations, edited by A. Quarteroni, Vol. 1697, Lecture Notes in Mathematics, Springer, New York, 1998, pp. 325-432.
-
(1998)
Advanced Numerical Approximation of Nonlinear Hyperbolic Equations
, vol.1697
, pp. 325-432
-
-
Shu, C.W.1
-
16
-
-
0003361172
-
Aerofoil RAE 2822: Pressure distributions, and boundary layer and wake measurements
-
Jan.
-
Cook, P. H., McDonald, M. A., and Firmin, M. C. P., "Aerofoil RAE 2822: Pressure Distributions, and Boundary Layer and Wake Measurements," Experimental Data Base for Computer Program Assessment, AGARD, Rept. AR 138, Jan. 1979.
-
(1979)
Experimental Data Base for Computer Program Assessment, AGARD, Rept. AR 138
-
-
Cook, P.H.1
McDonald, M.A.2
Firmin, M.C.P.3
-
17
-
-
73349090692
-
-
Ph.D. Dissertation (in Preparation), School of Aerospace Engineering, Georgia Inst. of Technology, Atlanta, GA, June
-
Min, B. Y., "A Physics Based Investigation of Gurney Flaps for Enhancement of Rotorcraft Flight Characteristics," Ph.D. Dissertation (in Preparation), School of Aerospace Engineering, Georgia Inst. of Technology, Atlanta, GA, June 2009
-
(2009)
A Physics Based Investigation of Gurney Flaps for Enhancement of Rotorcraft Flight Characteristics
-
-
Min, B.Y.1
-
18
-
-
73349132802
-
Full-reynolds stress modeling of circulation control airfoils
-
NASA CP 2005-213509/PT1 June
-
Chang, P. A., Slomski, J., Marino, T., Ebert, M. P., and Abramson, J., "Full-Reynolds Stress Modeling of Circulation Control Airfoils," Proceedings of the 2004 NASA/ONR Circulation Control Workshop, NASA CP 2005-213509/PT1 June 2005, pp. 141-166.
-
(2005)
Proceedings of the 2004 NASA/ONR Circulation Control Workshop
, pp. 141-166
-
-
Chang, P.A.1
Slomski, J.2
Marino, T.3
Ebert, M.P.4
Abramson, J.5
|