-
1
-
-
3042735005
-
Flow control using various plasma and aerodynamic approaches
-
doi:10.1016/j.ast.2004.01.005
-
Fomin, V. M., Tretyakov, P. K., and Taran, J.-P., "Flow Control Using Various Plasma and Aerodynamic Approaches," Aerospace Science and Technology, Vol.8, No.5, 2004, pp. 411-421. doi:10.1016/j.ast.2004.01.005
-
(2004)
Aerospace Science and Technology
, vol.8
, Issue.5
, pp. 411-421
-
-
Fomin, V.M.1
Tretyakov, P.K.2
Taran, J.-P.3
-
2
-
-
32844469699
-
Mechanisms of plasma actuators for hypersonic flow control
-
DOI 10.1016/j.paerosci.2005.11.001, PII S0376042105001235
-
Shang, J. S., Surzhikov, S. T., Kimmel, R., Gaitonde, D., Menart, J., and Hayes, J., "Mechanisms of Plasma Actuators for Hypersonic Flow Control," Progress in Aerospace Sciences, Vol.41, No.8, 2005, pp. 642-668. doi:10.1016/j.paerosci.2005.11.001 (Pubitemid 43255300)
-
(2005)
Progress in Aerospace Sciences
, vol.41
, Issue.8
, pp. 642-668
-
-
Shang, J.S.1
Surzhikov, S.T.2
Kimmel, R.3
Gaitonde, D.4
Menart, J.5
Hayes, J.6
-
3
-
-
0028424069
-
Aerodynamically blunt and sharp bodies
-
doi:10.2514/3.26449
-
Mason, W. H., and Lee, J., "Aerodynamically Blunt and Sharp Bodies," Journal of Spacecraft and Rockets, Vol.31, No.3, 1994, pp. 378-382. doi:10.2514/3.26449
-
(1994)
Journal of Spacecraft and Rockets
, vol.31
, Issue.3
, pp. 378-382
-
-
Mason, W.H.1
Lee, J.2
-
4
-
-
24144486241
-
Aerothermodynamic performance analysis of hypersonic flow on power law leading edges
-
Santos,W.F.N.,andLewis,M.J.," AerothermodynamicPerformanceAnalysisofHypersonicFlowonPowerLawLeadingEdges, "JournalofSpacecraftandRockets,Vol.42,No.4,2005,588-597.doi:10.2514/1. 9550(Pubitemid41229731)
-
(2005)
Journal of Spacecraft and Rockets
, vol.42
, Issue.4
, pp. 588-597
-
-
Santos, W.F.N.1
Lewis, M.J.2
-
5
-
-
0036576592
-
Hypersonic flow over a blunt body with plasma injection
-
Shang,J.S.,Hayes,J.,andMenart,J.," HypersonicFlowoveraBluntBodywithPlasmaInjection," JournalofSpacecraftandRockets,Vol.39,No.3,2002,367-375.doi:10.2514/2. 3835(Pubitemid34711699)
-
(2002)
Journal of Spacecraft and Rockets
, vol.39
, Issue.3
, pp. 367-375
-
-
Shang, J.S.1
Hayes, J.2
Menart, J.3
-
6
-
-
33748328030
-
Computational study of shock mitigation and drag reduction by pulsed energy lines
-
Kremeyer,K.,Sebastian,K.,andShu,C.-W.," ComputationalStudyofShockMitigationandDragReductionbyPulsedEnergyLines, "AIAAJournal,Vol.44,No.8,2006,1720-1731.doi:10.2514/1. 17854(Pubitemid44326533)
-
(2006)
AIAA Journal
, vol.44
, Issue.8
, pp. 1720-1731
-
-
Kremeyer, K.1
Sebastian, K.2
Shu, C.-W.3
-
7
-
-
34250755640
-
Control of edney IV interaction by energy pulse
-
Jan.
-
Yan, H., and Gaitonde, D., "Control of Edney IV Interaction by Energy Pulse," AIAA Paper 06-562, Jan. 2006.
-
(2006)
AIAA Paper
, vol.6
, Issue.562
-
-
Yan, H.1
Gaitonde, D.2
-
8
-
-
0033879314
-
Hypersonic flow control using upstream focused energy deposition
-
Riggins,D.W.,andNelson,H.F.," HypersonicFlowControlUsingUpstreamFocusedEnergyDeposition,"AIAAJournal,Vol. 38,No.4,2000,723-725.doi:10.2514/2.1020(Pubitemid30584749)
-
(2000)
AIAA Journal
, vol.38
, Issue.4
, pp. 723-725
-
-
Riggins, D.W.1
Nelson, H.F.2
-
9
-
-
0036156949
-
Magnetohydrodynamic control of hypersonic flows and scramjet inlets using electron beam ionization
-
Macheret,S.O.,Shneider,M.N.,andMiles,R.B.," MagnetohydrodynamicControlofHypersonic FlowsandScramjetInletsUsingElectronBeamIonization,"AIAAJournal,Vol.40,No.1, 2002,74-81.doi:10.2514/2.1616(Pubitemid34108730)
-
(2002)
AIAA Journal
, vol.40
, Issue.1
, pp. 74-81
-
-
Macheret, S.O.1
Shneider, M.N.2
Miles, R.B.3
-
10
-
-
54949113775
-
Hypersonic flow control using surface plasma actuator
-
doi:10.2514/1.24413
-
Shang, J. S., Kimmel, R. L., Menart, J., and Surzhikov, S. T., "Hypersonic Flow Control Using Surface Plasma Actuator," Journal of Propulsion and Power, Vol.24, No.5, 2008, pp. 923-934. doi:10.2514/1.24413
-
(2008)
Journal of Propulsion and Power
, vol.24
, Issue.5
, pp. 923-934
-
-
Shang, J.S.1
Kimmel, R.L.2
Menart, J.3
Surzhikov, S.T.4
-
11
-
-
77958137052
-
Creation of steering moments in supersonic flow by off-axis plasma heat addition
-
Jan.
-
Girgis, I. G., Shneider, M. N., Macheret, S. O., Brown, G. L., and Miles, R. B., "Creation of Steering Moments in Supersonic Flow by Off-Axis Plasma Heat Addition," AIAA Paper 02-129, Jan. 2002.
-
(2002)
AIAA Paper
, vol.2
, Issue.129
-
-
Girgis, I.G.1
Shneider, M.N.2
Macheret, S.O.3
Brown, G.L.4
Miles, R.B.5
-
12
-
-
45849153053
-
Feasibility study for steering a supersonic projectile by a plasma actuator
-
doi:10.2514/1.24696
-
Gnemmi, P., Charon, R., Dupéroux, J.-P., and George, A., "Feasibility Study for Steering a Supersonic Projectile by a Plasma Actuator," AIAA Journal, Vol.46, No.6, 2008, pp. 1308-1317. doi:10.2514/1.24696
-
(2008)
AIAA Journal
, vol.46
, Issue.6
, pp. 1308-1317
-
-
Gnemmi, P.1
Charon, R.2
Dupéroux, J.-P.3
George, A.4
-
13
-
-
34250743578
-
Study of plasma electrode arrangements for optimum lift in a Mach 5 flow
-
Jan.
-
Menart, J., Stanfield, S., Shang, J., Kimmel, R., and Hayes, J., "Study of Plasma Electrode Arrangements for Optimum Lift in a Mach 5 Flow," AIAA Paper 06-1172, Jan. 2006.
-
(2006)
AIAA Paper
, vol.6
, Issue.1172
-
-
Menart, J.1
Stanfield, S.2
Shang, J.3
Kimmel, R.4
Hayes, J.5
-
14
-
-
30744464871
-
Hypersonic separated flow control using magneto-aerodynamic interaction
-
Jan.
-
Updike, G. A., Shang, J. S., and Gaitonde, D. V., "Hypersonic Separated Flow Control Using Magneto-Aerodynamic Interaction," AIAA Paper 05-164, Jan. 2005.
-
(2005)
AIAA Paper
, vol.5
, Issue.164
-
-
Updike, G.A.1
Shang, J.S.2
Gaitonde, D.V.3
-
15
-
-
34250864458
-
Surface discharge for high-speed boundary layer control
-
Jan.
-
Kimmel, R. L., Hayes, J. R., Crafton., J. W., Fonov, S. D., Menart, J., and Shang, J., "Surface Discharge for High-Speed Boundary Layer Control," AIAA Paper 06-710, Jan. 2006.
-
(2006)
AIAA Paper
, vol.6
, Issue.710
-
-
Kimmel, R.L.1
Hayes, J.R.2
Crafton, J.W.3
Fonov, S.D.4
Menart, J.5
Shang, J.6
-
16
-
-
30744434640
-
Plasma-enhanced hypersonic performance enabled by MHD power extraction
-
Jan.
-
Miles, R. B., Macheret, S. O., Shneider, M. N., Steeves, C., Murray, R. C., Smith, T., and Zaidi, S. H., "Plasma-Enhanced Hypersonic Performance Enabled by MHD Power Extraction," AIAA Paper 05561, Jan. 2005.
-
(2005)
AIAA Paper
, vol.5
, Issue.561
-
-
Miles, R.B.1
Macheret, S.O.2
Shneider, M.N.3
Steeves, C.4
Murray, R.C.5
Smith, T.6
Zaidi, S.H.7
-
17
-
-
85088719970
-
Development of an unstructured navier-stokes solver for hypersonic nonequilibrium aerothermodynamics
-
June
-
Scalabrin, L. C., and Boyd, I. D., "Development of an Unstructured Navier-Stokes Solver For Hypersonic Nonequilibrium Aerothermodynamics," AIAA Paper 05-5203, June 2005.
-
(2005)
AIAA Paper
, vol.5
, Issue.5203
-
-
Scalabrin, L.C.1
Boyd, I.D.2
-
18
-
-
33845519493
-
Numerical simulation of weakly ionized hypersonic flow for reentry configurations
-
June
-
Scalabrin, L. C., and Boyd, I. D., "Numerical Simulation of Weakly Ionized Hypersonic Flow for Reentry Configurations," AIAA Paper 063773, June 2006.
-
(2006)
AIAA Paper
, vol.6
, Issue.3773
-
-
Scalabrin, L.C.1
Boyd, I.D.2
-
19
-
-
35748970751
-
Numerical simulation of the FIRE-II convective and radiative heating rates
-
June
-
Scalabrin, L. C., and Boyd, I. D., "Numerical Simulation of the FIRE-II Convective and Radiative Heating Rates," AIAA Paper 07-4044, June 2007.
-
(2007)
AIAA Paper
, vol.7
, Issue.4044
-
-
Scalabrin, L.C.1
Boyd, I.D.2
-
21
-
-
33845457638
-
Plasma-based hypersonic flow control
-
June
-
Poggie, J., "Plasma-Based Hypersonic Flow Control," AIAA Paper 063567, June 2006.
-
(2006)
AIAA Paper
, vol.6
, Issue.3567
-
-
Poggie, J.1
-
22
-
-
0033197306
-
Laminar-turbulent transition in a Mach 8 elliptic cone flow
-
doi:10.2514/2.836
-
Kimmel, R. L., Poggie, J., and Schwoerke, S. N., "Laminar-Turbulent Transition in a Mach 8 Elliptic Cone Flow," AIAA Journal, Vol.37, No.9, 1999, pp. 1080-1087. doi:10.2514/2.836
-
(1999)
AIAA Journal
, vol.37
, Issue.9
, pp. 1080-1087
-
-
Kimmel, R.L.1
Poggie, J.2
Schwoerke, S.N.3
-
23
-
-
0031186560
-
Three-dimensional hypersonic laminar boundary-layer computations for transition experiment design
-
Kimmel,R.,Klein,M.,andSchwoerke,S.,"Three- DimensionalHypersonicLaminarBoundary- LayerComputationsforTransitionExperimentDesign,"AIAAJournal,Vol.34,No.4, 1997,409-415.(Pubitemid127579015)
-
(1997)
Journal of Spacecraft and Rockets
, vol.34
, Issue.4
, pp. 409-415
-
-
Kimmel, R.L.1
Klein, M.A.2
Schwoerke, S.N.3
-
24
-
-
35748933540
-
Unstructured grid approaches for accurate aeroheating simulations
-
June
-
Candler, G., "Unstructured Grid Approaches for Accurate Aeroheating Simulations," AIAA Paper 07-3959, June 2007.
-
(2007)
AIAA Paper
, vol.7
, Issue.3959
-
-
Candler, G.1
-
25
-
-
77958134328
-
Numerical study of energy deposition requirements for aerodynamic control of hypersonic vehicles
-
Jan.
-
Bisek, N. J., Boyd, I. D., and Poggie, J., "Numerical Study of Energy Deposition Requirements for Aerodynamic Control of Hypersonic Vehicles," AIAA Paper 08-1109, Jan. 2008.
-
(2008)
AIAA Paper
, vol.8
, Issue.1109
-
-
Bisek, N.J.1
Boyd, I.D.2
Poggie, J.3
-
26
-
-
67650963651
-
-
Cornell Aeronautical Laboratory, Inc., Rept. AM-1800-Y-2, Buffalo, NY, Dec. ASC 94 2649
-
Nowlan, D., Burke, A., and Bird, K., "Pressure and Heat Transfer Distribution on ASD Elliptic Cone (W3) and ASD Sortie (W4) in the CAL 48-Inch Hypersonic Shock Tunnel," Cornell Aeronautical Laboratory, Inc., Rept. AM-1800-Y-2, Buffalo, NY, Dec. 1963, ASC 94 2649.
-
(1963)
Pressure and Heat Transfer Distribution on ASD Elliptic Cone (W3) and ASD Sortie (W4) in the CAL 48-Inch Hypersonic Shock Tunnel
-
-
Nowlan, D.1
Burke, A.2
Bird, K.3
-
27
-
-
0346846524
-
Effect of vibrational nonequilibrium on hypersonic double-cone experiments
-
doi:10.2514/2.6834
-
Nompelis, I., Candler, G., and Holden, M., "Effect of Vibrational Nonequilibrium on Hypersonic Double-Cone Experiments," AIAA Journal, Vol.41, No.11, 2003, pp. 2162-2169. doi:10.2514/2.6834
-
(2003)
AIAA Journal
, vol.41
, Issue.11
, pp. 2162-2169
-
-
Nompelis, I.1
Candler, G.2
Holden, M.3
-
28
-
-
29044431641
-
Falcon hypersonic technology overview
-
May
-
Walker, S. H., and Rodgers, F., "Falcon Hypersonic Technology Overview," AIAA Paper 05-3253, May 2005.
-
(2005)
AIAA Paper
, vol.5
, Issue.3253
-
-
Walker, S.H.1
Rodgers, F.2
-
29
-
-
2942752086
-
Effect of surface plasma discharges on boundary layers at Mach 5
-
Jan.
-
Kimmel, R. L., Hayes, J. R., Menart, J. A., and Shang, J., "Effect of Surface Plasma Discharges on Boundary Layers at Mach 5," AIAA Paper 04-509, Jan. 2004.
-
(2004)
AIAA Paper
, vol.4
, Issue.509
-
-
Kimmel, R.L.1
Hayes, J.R.2
Menart, J.A.3
Shang, J.4
-
30
-
-
67650944952
-
-
U.S. Air Force Research Laboratory, Rept ARFL-VA-WP-TR-2006-3006, Wright-Patterson AFB, OH, Dec. AFRL/WS 06-0097
-
Kimmel, R., Hayes, J., Menart, J., and Shang, J., "Supersonic Plasma Flow Control Experiments," U.S. Air Force Research Laboratory, Rept ARFL-VA-WP-TR-2006-3006, Wright-Patterson AFB, OH, Dec. 2005, AFRL/WS 06-0097.
-
(2005)
Supersonic Plasma Flow Control Experiments
-
-
Kimmel, R.1
Hayes, J.2
Menart, J.3
Shang, J.4
-
31
-
-
67650970029
-
-
Aviation Week and Space Technology, March
-
Velocci, A. L. J., "A General Atomics-Led Team," Aviation Week and Space Technology, March 2007, p. 36.
-
(2007)
A General Atomics-Led Team
, pp. 36
-
-
Velocci, A.L.J.1
-
32
-
-
78049490320
-
Numerical study of plasma assisted aerodynamic control for hypersonic vehicles
-
June
-
Bisek, N. J., Boyd, I. D., and Poggie, J., "Numerical Study of Plasma Assisted Aerodynamic Control for Hypersonic Vehicles," AIAA Paper 08-4226, June 2008.
-
(2008)
AIAA Paper
, vol.8
, Issue.4226
-
-
Bisek, N.J.1
Boyd, I.D.2
Poggie, J.3
|