-
2
-
-
84896885777
-
Snapshot of Active Flow Control Research at NASA Langley
-
st Flow Control Conference, St. Louis, MO, June
-
Washburn, A. E., Gorton, S. Althoff, and Anders, S. G.: "Snapshot of Active Flow Control Research at NASA Langley", AIAA Paper 2002-3155, AIAA 1st Flow Control Conference, St. Louis, MO, 24-27 June 2002.
-
(2002)
AIAA Paper 2002-3155
, pp. 24-27
-
-
Washburn, A.E.1
Gorton, S.2
Althoff3
Anders, S.G.4
-
4
-
-
0343911306
-
Control of Turbulent Boundary Layer Separation using Micro-Vortex Generators
-
30th AIAA Fluid Dynamics Conference, Norfolk, VA, June-1 July
-
Lin, John C.: "Control of Turbulent Boundary Layer Separation using Micro-Vortex Generators", AIAA Paper 99-3404, 30th AIAA Fluid Dynamics Conference, Norfolk, VA,.28 June-1 July, 1999.
-
(1999)
AIAA Paper 99-3404
, vol.28
-
-
Lin, J.C.1
-
5
-
-
0034291016
-
The Control of Flow Separation by Periodic Excitation
-
Greenblatt, David, and Wygnanski, Israel, J.: "The Control of Flow Separation by Periodic Excitation", Progress in Aerospace Sciences 36 (2000) 487-545.
-
(2000)
Progress In Aerospace Sciences
, vol.36
, pp. 487-545
-
-
Greenblatt, D.1
Wygnanski, I.2
-
6
-
-
84982318346
-
Oscillatory Control of Separation at High Reynolds Number
-
AIAA Aerospace Sciences Meeting & Exhibit, 36th, Reno, NV, Jan
-
Seifert, A., and Pack, L. G.: "Oscillatory Control of Separation at High Reynolds Number", AIAA Paper 98-0214, AIAA Aerospace Sciences Meeting & Exhibit, 36th, Reno, NV, Jan. 12-15, 1998.
-
(1998)
AIAA Paper 98-0214
, pp. 12-15
-
-
Seifert, A.1
Pack, L.G.2
-
7
-
-
0003238760
-
Oscillatory Excitation of Unsteady Compressible Flows over Airfoils at Flight Reynolds Numbers
-
Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan
-
Seifert, Avi, and Pack, LaTunia G.: "Oscillatory Excitation of Unsteady Compressible Flows over Airfoils at Flight Reynolds Numbers", AIAA Paper 99-0925, Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan. 11-14, 1999.
-
(1999)
AIAA Paper 99-0925
, pp. 11-14
-
-
Seifert, A.1
Pack, L.G.2
-
8
-
-
84963730203
-
Active Control of Separated Flows on Generic Configurations at High Reynolds Numbers
-
AIAA Fluid Dynamics Conference, 30th, Norfolk, VA, June 28-July
-
Seifert, Avi, and Pack, LaTunia: "Active Control of Separated Flows on Generic Configurations at High Reynolds Numbers", AIAA Paper 99-3403, AIAA Fluid Dynamics Conference, 30th, Norfolk, VA, June 28-July 1, 1999.
-
(1999)
AIAA Paper 99-3403
, pp. 1
-
-
Seifert, A.1
Pack, L.2
-
9
-
-
85087602966
-
Dynamics of Active Separation Control at High Reynolds Numbers
-
AIAA Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan
-
Pack, LaTunia, and Seifert, Avi: "Dynamics of Active Separation Control at High Reynolds Numbers", AIAA Paper 2000-0409, AIAA Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000.
-
(2000)
AIAA Paper 2000-0409
, pp. 10-13
-
-
Pack, L.1
Seifert, A.2
-
10
-
-
84894314019
-
Sweep and Compressibility Effects on Active Separation Control at High Reynolds Numbers
-
AIAA Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan
-
Seifert, Avi, and Pack, LaTunia G.: "Sweep and Compressibility Effects on Active Separation Control at High Reynolds Numbers", AIAA Paper 2000-0410, AIAA Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000.
-
(2000)
AIAA Paper 2000-0410
, pp. 10-13
-
-
Seifert, A.1
Pack, L.G.2
-
11
-
-
85087594666
-
Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions
-
Fluids. 2000 Conference and Exhibit, Denver, CO, June
-
Seifert, Avi, and Pack, LaTunia G.: "Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions", AIAA Paper 2000-2542, Fluids. 2000 Conference and Exhibit, Denver, CO, June 19-22, 2000.
-
(2000)
AIAA Paper 2000-2542
, pp. 19-22
-
-
Seifert, A.1
Pack, L.G.2
-
12
-
-
84896693324
-
Active Control of Flow Separation from the Slat Shoulder of a Supercritical Airfoil
-
AIAA 1st Flow Control Conference, St. Louis, MO, June
-
Pack, LaTunia, G., Schaeffler, Norman W., Yao, Chung-Sheng, and Seifert, Avi: "Active Control of Flow Separation from the Slat Shoulder of a Supercritical Airfoil", AIAA Paper 2002-3156, AIAA 1st Flow Control Conference, St. Louis, MO, 24-27 June 2002.
-
(2002)
AIAA Paper 2002-3156
, pp. 24-27
-
-
Pack, L.G.1
Schaeffler, N.W.2
Yao, C.-S.3
Seifert, A.4
-
13
-
-
0003236011
-
Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft
-
June
-
McLean, J.D., Crouch, J. D., Stoner, R. C, Sakurai, G. E., Seidel, G. E., Feifel, W. M., and Rush, H. M.: "Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft", NASA CR-1999- 209338, June 1999.
-
(1999)
NASA CR-1999- 209338
-
-
McLean, J.D.1
Crouch, J.D.2
Stoner, R.C.3
Sakurai, G.E.4
Seidel, G.E.5
Feifel, W.M.6
Rush, H.M.7
-
14
-
-
0003247184
-
Evolution, Calibration, and Operational Characteristics of the Two-Dimensional Test Section of the Langley 0.3-meter Transonic Cryo Tunnel
-
Ladson, C. A. and Ray, E. J.: "Evolution, Calibration, and Operational Characteristics of the Two-Dimensional Test Section of the Langley 0.3-meter Transonic Cryo Tunnel", NASA TP-2749, 1987.
-
(1987)
NASA TP-2749
-
-
Ladson, C.A.1
Ray, E.J.2
-
15
-
-
0003212126
-
Operating Envelope Charts for the Langley 0.3-meter Transonic Cryogenic Wind Tunnel
-
Rallo, R. A., Dress, D. A., and Siegle, H. J. A.: "Operating Envelope Charts for the Langley 0.3-meter Transonic Cryogenic Wind Tunnel", NASA TM-89008, 1986.
-
(1986)
NASA TM-89008
-
-
Rallo, R.A.1
Dress, D.A.2
Siegle, H.J.A.3
-
16
-
-
0031192966
-
Parametric Investigation of a High-Lift Airfoil at High Reynolds Numbers
-
Lin, J. C. and Dominik, C. J.: "Parametric Investigation of a High-Lift Airfoil at High Reynolds Numbers", Journal of Aircraft, Vol. 33, No. 4, 1997, pp. 485-491.
-
(1997)
Journal of Aircraft
, vol.33
, Issue.4
, pp. 485-491
-
-
Lin, J.C.1
Dominik, C.J.2
-
17
-
-
85086616041
-
An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications
-
st AIAA Flow Control Conference, St. Louis, MO, June
-
Jones, G. S., Viken, S. A. Washburn, A.E. Jenkins, L. N. Cagle, C.M., "An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications," AIAA Paper 2002-3157, 1st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002.
-
(2002)
AIAA Paper 2002-3157
, pp. 24-27
-
-
Jones, G.S.1
Viken, S.A.2
Washburn, A.E.3
Jenkins, L.N.4
Cagle, C.M.5
-
18
-
-
0021857058
-
Circulation Control Airfoils Past, Present, and Future
-
January
-
Wood, N., and J. Nielson, "Circulation Control Airfoils Past, Present, and Future," AIAA Paper 850204, January, 1985.
-
(1985)
AIAA Paper 850204
-
-
Wood, N.1
Nielson, J.2
-
19
-
-
85068439731
-
Circulation control Pneumatic Aerodynamics: Blown force and Moment Augmentation and Modifications; Past, Present, & Future
-
June
-
Englar, R.J., Circulation control Pneumatic Aerodynamics: blown force and Moment Augmentation and Modifications; Past, Present, & Future", AIAA 2000-2541, June 2000.
-
(2000)
AIAA
, pp. 2000-2541
-
-
Englar, R.J.1
-
20
-
-
85086492045
-
Numerical Simulations of the Steady and Unsteady Aerodynamic Characteristics of a Circulation control Wing Airfoil
-
0704, January
-
Liu, Y., Sankar, L.N., Englar, R.J., Ahuja, K.K., "Numerical Simulations of the Steady and Unsteady Aerodynamic Characteristics of a Circulation control Wing Airfoil," AIAA 2001-0704, January 2001.
-
(2001)
AIAA
, pp. 2001
-
-
Liu, Y.1
Sankar, L.N.2
Englar, R.J.3
Ahuja, K.K.4
-
21
-
-
33845586028
-
On the Phenomenon of Fluid Veins and their Application, the Coanda Effect
-
F-TS-786-RE
-
Metral, A.R., "On the Phenomenon of Fluid Veins and their Application, the Coanda Effect," AF Translation, F-TS-786-RE, 1939.
-
(1939)
AF Translation
-
-
Metral, A.R.1
-
23
-
-
33845275612
-
A Wind Tunnel Model to Explore Unsteady Circulation Control for General Aviation Applications
-
st AIAA Flow Control Conference, St. Louis, MO, June
-
Cagle, C.M., Jones, G.S. "A Wind Tunnel Model to Explore Unsteady Circulation Control for General Aviation Applications, AIAA 2002-3240, 1st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002.
-
(2002)
AIAA 2002-3240
, pp. 24-27
-
-
Cagle, C.M.1
Jones, G.S.2
-
24
-
-
84894624689
-
-
Honeywell Document No. 12081- FR1, July
-
Rose, R.E., Hammer, J.M., & Kizilos, A.P., "Feasibility Study of a Bi-directional Jet Flap Device for Application to Helicopter Rotor Blades," Honeywell Document No. 12081- FR1, July 1971.
-
(1971)
Feasibility Study of a Bi-directional Jet Flap Device For Application to Helicopter Rotor Blades
-
-
Rose, R.E.1
Hammer, J.M.2
Kizilos, A.P.3
-
25
-
-
2942717973
-
Design of a Circulation Control Stern Plane for Submarine Applications
-
March
-
Englar, R.J., Williams, R.M., "Design of a Circulation Control Stern Plane for Submarine Applications," NSRDC Technical Note AL-200, March 1971.
-
(1971)
NSRDC Technical Note AL-200
-
-
Englar, R.J.1
Williams, R.M.2
-
26
-
-
84894619105
-
Overview of Active Flow Control Actuator Development at NASA Langley Research Center
-
1st AIAA Flow Control Conference, St. Louis, MO, June
-
Schaeffler, N.W., Hepner, T.E., Jones, G.S., Kegerise, M.A., "Overview of Active Flow Control Actuator Development at NASA Langley Research Center," AIAA 2002-3159, 1st AIAA Flow Control Conference, St. Louis, MO, 24-27 June 2002.
-
(2002)
AIAA 2002-3159
, pp. 24-27
-
-
Schaeffler, N.W.1
Hepner, T.E.2
Jones, G.S.3
Kegerise, M.A.4
-
27
-
-
27644484832
-
Langley Full-Scale- Tunnel Tests of the Custer Channel Wing Airplane
-
National Advisory Committee for Aeronautics, April
-
Pasamanick, Jerome, "Langley Full-Scale- Tunnel Tests of the Custer Channel Wing Airplane," NACA RM L53A09, National Advisory Committee for Aeronautics, April, 1953.
-
(1953)
NACA RM L53A09
-
-
Pasamanick, J.1
-
28
-
-
85085402933
-
Pneumatic Channel Wing Power-Lift Advanced Super-STOL Aircraft
-
1st AIAA Flow Control Conference, St. Louis, MO, June
-
Englar, Robert J., and Campbell, Bryan A.: "Pneumatic Channel Wing Power-Lift Advanced Super-STOL Aircraft", AIAA Paper 2002-3275, 1st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002.
-
(2002)
AIAA Paper 2002-3275
, pp. 24-27
-
-
Englar, R.J.1
Campbell, B.A.2
-
29
-
-
85085402933
-
Pneumatic Channel Wing Power-Lift Advanced Super-STOL Aircraft
-
1st AIAA Flow Control Conference, St. Louis, MO, June
-
Englar, Robert J., and Campbell, Bryan A.: "Pneumatic Channel Wing Power-Lift Advanced Super-STOL Aircraft", AIAA Paper 2002-3275, 1st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002
-
(2002)
AIAA Paper 2002-3275
, pp. 24-27
-
-
Englar, R.J.1
Campbell, B.A.2
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