-
1
-
-
0004079116
-
-
AIAA, Reston, VA, 2nd ed.
-
Anderson, J. D., Jr., Hypersonic and High-Temperature Gas Dynamics, AIAA, Reston, VA, 2nd ed., 2006.
-
(2006)
Hypersonic and High-temperature Gas Dynamics
-
-
Anderson Jr., J.D.1
-
2
-
-
79251501159
-
Reusable space vehicles: Lessons from four decades of futility
-
Jan
-
Bille, M., Williams, T., and Villhard, V., "Reusable Space Vehicles: Lessons From Four Decades of Futility", AIAA Paper 2003-659, Jan. 2003.
-
(2003)
AIAA Paper 2003-659
-
-
Bille, M.1
Williams, T.2
Villhard, V.3
-
3
-
-
35748930889
-
Fundamental aeronautics hypersonics project: Overview
-
June
-
Mansour, N., Pittman, J., and Olson, L., "Fundamental Aeronautics Hypersonics Project: Overview", AIAA Paper 2007-4263, June 2007.
-
(2007)
AIAA Paper 2007-4263
-
-
Mansour, N.1
Pittman, J.2
Olson, L.3
-
4
-
-
29044436983
-
Airbreathing hypersonic propulsion at pratt and whitney-overview
-
May
-
Kazmar, R., "Airbreathing Hypersonic Propulsion at Pratt and Whitney-Overview", AIAA Paper 2005-3256, May 2005.
-
(2005)
AIAA Paper 2005-3256
-
-
Kazmar, R.1
-
6
-
-
77958459428
-
Hypersonic international flight research and experimentation (HIFiRE) fundamental sciences and technology development strategy
-
April-May
-
Dolvin, D. J., "Hypersonic International Flight Research and Experimentation (HIFiRE) Fundamental Sciences and Technology Development Strategy", AIAA Paper 2008-2581, April-May 2008.
-
(2008)
AIAA Paper 2008-2581
-
-
Dolvin, D.J.1
-
7
-
-
34250699512
-
X-43 scramjet power breaks the hypersonic barrier: Dryden lectureship in research for 2006
-
Jan
-
McClinton, C., "X-43 Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006", AIAA Paper 2006-1, Jan. 2006.
-
(2006)
AIAA Paper 2006-1
-
-
McClinton, C.1
-
8
-
-
79251493166
-
Development of the hyshot stability demonstrator
-
April
-
Neuenhahn, T., Olivier, H., and Paull, A., "Development of the Hyshot Stability Demonstrator", AIAA Paper 2006-2960, April 1995.
-
(1995)
AIAA Paper 2006-2960
-
-
Neuenhahn, T.1
Olivier, H.2
Paull, A.3
-
9
-
-
34248368556
-
Nonlinear longitudinal dynamic model of an air-breathing hypersonic vehicle
-
March-April, doi:10.2514/1.23370
-
Bolender, M. A., and Doman, D. B., "Nonlinear Longitudinal Dynamic Model of an Air-Breathing Hypersonic Vehicle", Journal of Spacecraft and Rockets, Vol. 44, No. 2, March-April 2007, pp. 374-387. doi:10.2514/1.23370
-
(2007)
Journal of Spacecraft and Rockets
, vol.44
, Issue.2
, pp. 374-387
-
-
Bolender, M.A.1
Doman, D.B.2
-
10
-
-
77956764593
-
The joint technology office on hypersonics
-
April
-
Ouzts, P., "The Joint Technology Office on Hypersonics", AIAA Paper 2008-2576, April 2008.
-
(2008)
AIAA Paper 2008-2576
-
-
Ouzts, P.1
-
11
-
-
77049120349
-
On the use of reduced-order models for a shallow curved beam under combined loading
-
April
-
Spottswood, S. M., Hollkamp, J. J., and Eason, T. G., "On the Use of Reduced-Order Models for a Shallow Curved Beam Under Combined Loading", AIAA Paper 2008-2235, April 2008.
-
(2008)
AIAA Paper 2008-2235
-
-
Spottswood, S.M.1
Hollkamp, J.J.2
Eason, T.G.3
-
12
-
-
0027190092
-
An overview of aeroelasticity studies for the national aero-space plane
-
April
-
Ricketts, R. H., Noll, T. E., Whitlow, W., Jr., and Huttsell, L. J., "An Overview of Aeroelasticity Studies for the National Aero-Space Plane", AIAA Paper 1993-1313, April 1993.
-
(1993)
AIAA Paper 1993-1313
-
-
Ricketts, R.H.1
Noll, T.E.2
Whitlow Jr., W.3
Huttsell, L.J.4
-
13
-
-
3042704414
-
CFD-based aeroelastic analysis of the X-43 hypersonic flight vehicle
-
Jan
-
Gupta, K. K., Voelker, L. S., Bach, C., Doyle, T., and Hahn, E., "CFD-Based Aeroelastic Analysis of the X-43 Hypersonic Flight Vehicle", AIAA Paper 2001-712, Jan. 2001.
-
(2001)
AIAA Paper 2001-712
-
-
Gupta, K.K.1
Voelker, L.S.2
Bach, C.3
Doyle, T.4
Hahn, E.5
-
14
-
-
2942723480
-
X-33 hypersonic boundary layer transition
-
June-July
-
Berry, S. A., Horvath, T. J., Hollis, B. R., Thompson, R. A., and Hamilton, H. H., "X-33 Hypersonic Boundary Layer Transition", AIAA Paper 1999-3560, June-July 1999.
-
(1999)
AIAA Paper 1999-3560
-
-
Berry, S.A.1
Horvath, T.J.2
Hollis, B.R.3
Thompson, R.A.4
Hamilton, H.H.5
-
15
-
-
85088358637
-
Aeroheating predictions for X-34 using an inviscid-boundary layer method
-
Jan
-
Riley, C. J., Kleb, W. L., and Alter, S. J., "Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method", AIAA Paper 1999-880, Jan. 1999.
-
(1999)
AIAA Paper 1999-880
-
-
Riley, C.J.1
Kleb, W.L.2
Alter, S.J.3
-
17
-
-
0142064537
-
Air-breathing hypersonic waveriders: A survey of research needs
-
University of Maryland, College Park, MD, Oct
-
Blankson, I. M., "Air-Breathing Hypersonic Waveriders: A Survey of Research Needs", Proceedings of the First International Waverider Symposium, University of Maryland, College Park, MD, Oct. 1990.
-
(1990)
Proceedings of the First International Waverider Symposium
-
-
Blankson, I.M.1
-
18
-
-
0142087653
-
Fifty years of hypersonics: Where we've been and where we're going
-
April, doi:10.1016/S0376-0421 03 00079-4
-
Bertin, J. J., and Cummings, R. M., "Fifty Years of Hypersonics: Where We've Been and Where We're Going", Progress in Aerospace Sciences, Vol. 39, April 2003, pp. 511-536. doi:10.1016/S0376-0421 (03) 00079-4
-
(2003)
Progress in Aerospace Sciences
, vol.39
, pp. 511-536
-
-
Bertin, J.J.1
Cummings, R.M.2
-
19
-
-
85088755077
-
Flight dynamics and control of air-breathing hypersonic vehicles: Review and new directions
-
Dec
-
Fidan, B., Mirmirani, M., and Ionnou, P., "Flight Dynamics and Control of Air-Breathing Hypersonic Vehicles: Review and New Directions", AIAA Paper 2003-7081, Dec. 2003.
-
(2003)
AIAA Paper 2003-7081
-
-
Fidan, B.1
Mirmirani, M.2
Ionnou, P.3
-
20
-
-
77956371879
-
Structural dynamic and aeroelastic considerations for hypersonic vehicles
-
April
-
Cazier, F. W., Doggett, R., and Ricketts, R. H., "Structural Dynamic and Aeroelastic Considerations for Hypersonic Vehicles", AIAA Paper 1991-1255, April 1991.
-
(1991)
AIAA Paper 1991-1255
-
-
Cazier, F.W.1
Doggett, R.2
Ricketts, R.H.3
-
21
-
-
54549111524
-
Similarity laws for aerothermoelastic testing
-
Aug
-
Dugundji, J., and Calligeros, J. M., "Similarity Laws for Aerothermoelastic Testing", Journal of the Aerospace Sciences, Vol. 29, No. 8, Aug. 1962, pp. 935-950.
-
(1962)
Journal of the Aerospace Sciences
, vol.29
, Issue.8
, pp. 935-950
-
-
Dugundji, J.1
Calligeros, J.M.2
-
22
-
-
0000458626
-
Oscillating airfoils at high mach numbers
-
June
-
Lighthill, M. J., "Oscillating Airfoils at High Mach Numbers", Journal of the Aeronautical Sciences, Vol. 20, No. 6, June 1953, pp. 402-406.
-
(1953)
Journal of the Aeronautical Sciences
, vol.20
, Issue.6
, pp. 402-406
-
-
Lighthill, M.J.1
-
23
-
-
0000051591
-
Piston theory - A new aerodynamic tool for the aeroelastician
-
Dec
-
Ashley, H., and Zartarian, G., "Piston Theory-A New Aerodynamic Tool for the Aeroelastician", Journal of the Aeronautical Sciences, Vol. 23, No. 12, Dec. 1956, pp. 1109-1118.
-
(1956)
Journal of the Aeronautical Sciences
, vol.23
, Issue.12
, pp. 1109-1118
-
-
Ashley, H.1
Zartarian, G.2
-
25
-
-
5244248456
-
-
NACA TN 4335
-
Morgan, H. G., Huckel, V., and Runyan, H. L., "Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparison with Experimental Results", NACA TN 4335, 1958.
-
(1958)
Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparison with Experimental Results
-
-
Morgan, H.G.1
Huckel, V.2
Runyan, H.L.3
-
26
-
-
33947260045
-
Dynamic airloads and aeroelastic problems at entry mach numbers
-
March
-
Zartarian, G., Hsu, P. T., and Ashley, H., "Dynamic Airloads and Aeroelastic Problems at Entry Mach Numbers", Journal of the Aeronautical Sciences, Vol. 28, No. 3, March 1961, pp. 209-222.
-
(1961)
Journal of the Aeronautical Sciences
, vol.28
, Issue.3
, pp. 209-222
-
-
Zartarian, G.1
Hsu, P.T.2
Ashley, H.3
-
27
-
-
0003090954
-
Theoretical considerations of flutter at high mach numbers
-
June
-
Morgan, H. G., Runyan, H. L., and Huckel, V., "Theoretical Considerations of Flutter at High Mach Numbers", Journal of the Aeronautical Sciences, Vol. 25, No. 6, June 1958, pp. 371-381.
-
(1958)
Journal of the Aeronautical Sciences
, vol.25
, Issue.6
, pp. 371-381
-
-
Morgan, H.G.1
Runyan, H.L.2
Huckel, V.3
-
28
-
-
0004186280
-
-
Wiley, New York
-
Bisplinghoff, R. L., and Ashley, H., Principles of Aeroelasticity, Wiley, New York, 1962.
-
(1962)
Principles of Aeroelasticity
-
-
Bisplinghoff, R.L.1
Ashley, H.2
-
29
-
-
0027205973
-
Aerothermoelastic analysis of a NASP demonstrator model
-
April
-
Heeg, J., Zeiler, T. A., Pototzky, A. S., Spain, C. V., and Engelund, W. C., "Aerothermoelastic Analysis of a NASP Demonstrator Model", AIAA Paper 1993-1366, April 1993.
-
(1993)
AIAA Paper 1993-1366
-
-
Heeg, J.1
Zeiler, T.A.2
Pototzky, A.S.3
Spain, C.V.4
Engelund, W.C.5
-
31
-
-
0029225020
-
Hypersonic panel flutter studies on curved panels
-
April
-
Nydick, I., Friedmann, P. P., and Zhong, X., "Hypersonic Panel Flutter Studies on Curved Panels", AIAA Paper 1995-1485, April 1995.
-
(1995)
AIAA Paper 1995-1485
-
-
Nydick, I.1
Friedmann, P.P.2
Zhong, X.3
-
32
-
-
0345914634
-
A flutter investigation of all-moveable NASP-like wings at hypersonic speeds
-
April
-
Spain, C. V., Zeiler, T. A., Bullock, E. P., and Hodge, J. S., "A Flutter Investigation of All-Moveable NASP-Like Wings at Hypersonic Speeds", AIAA Paper 1993-1315, April 1993.
-
(1993)
AIAA Paper 1993-1315
-
-
Spain, C.V.1
Zeiler, T.A.2
Bullock, E.P.3
Hodge, J.S.4
-
33
-
-
0031140542
-
From piston theory to a unified hypersonic-supersonic lifting surface method
-
May-June, doi:10.2514/2.2199
-
Liu, D. D., Yao, Z. X., Sarhaddi, D., and Chavez, F., "From Piston Theory to a Unified Hypersonic-Supersonic Lifting Surface Method", Journal of Aircraft, Vol. 34, No. 3, May-June 1997, pp. 304-312. doi:10.2514/2.2199
-
(1997)
Journal of Aircraft
, vol.34
, Issue.3
, pp. 304-312
-
-
Liu, D.D.1
Yao, Z.X.2
Sarhaddi, D.3
Chavez, F.4
-
34
-
-
54549087792
-
Aeroelastic and aerothermoelastic behavior in hypersonic flow
-
Oct, doi:10.2514/1.36711
-
McNamara, J. J., Friedmann, P. P., Powell, K. G., Thuruthimattam, B. J., and Bartels, R. E., "Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow", AIAA Journal, Vol. 46, No. 10, Oct. 2008, pp. 2591-2610. doi:10.2514/1.36711
-
(2008)
AIAA Journal
, vol.46
, Issue.10
, pp. 2591-2610
-
-
McNamara, J.J.1
Friedmann, P.P.2
Powell, K.G.3
Thuruthimattam, B.J.4
Bartels, R.E.5
-
35
-
-
77952246362
-
Computational aeroelastic studies of a generic hypersonic vehicle
-
Dec
-
Thuruthimattam, B. J., Friedmann, P. P., Powell, K. G., and Bartels, R. E., "Computational Aeroelastic Studies of a Generic Hypersonic Vehicle", The Aeronautical Journal, Vol. 113, No. 1150, Dec. 2009, pp. 763-774.
-
(2009)
The Aeronautical Journal
, vol.113
, Issue.1150
, pp. 763-774
-
-
Thuruthimattam, B.J.1
Friedmann, P.P.2
Powell, K.G.3
Bartels, R.E.4
-
36
-
-
0029696941
-
Quasisteady aerodynamics for flutter analysis using steady computational fluid dynamics calculations
-
Jan.-Feb, doi:10.2514/3.46921
-
Scott, R. C., and Pototzky, A. S., "Quasisteady Aerodynamics for Flutter Analysis Using Steady Computational Fluid Dynamics Calculations", Journal of Aircraft, Vol. 33, No. 1, Jan.-Feb. 1996, pp. 191-197. doi:10.2514/3.46921
-
(1996)
Journal of Aircraft
, vol.33
, Issue.1
, pp. 191-197
-
-
Scott, R.C.1
Pototzky, A.S.2
-
37
-
-
84855621533
-
A reduced order aerothermodynamic modeling framework for hypersonic aerothermoelasticity
-
April
-
Crowell, A. R., McNamara, J. J., Kecskemety, K. M., and Goerig, T., "A Reduced Order Aerothermodynamic Modeling Framework for Hypersonic Aerothermoelasticity", AIAA Paper 2010-2969, April 2010.
-
(2010)
AIAA Paper 2010-2969
-
-
Crowell, A.R.1
McNamara, J.J.2
Kecskemety, K.M.3
Goerig, T.4
-
38
-
-
0004230787
-
-
Addison-Wesley, Cambridge, MA
-
Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Addison-Wesley, Cambridge, MA, 1955.
-
(1955)
Aeroelasticity
-
-
Bisplinghoff, R.L.1
Ashley, H.2
Halfman, R.L.3
-
39
-
-
77958557343
-
Approximate modeling of unsteady aerodynamic loads in hypersonic aeroelasticity
-
Stockholm, June
-
McNamara, J. J., Gogulapati, A., Friedmann, P. P., and Banavara, N. K., "Approximate Modeling of Unsteady Aerodynamic Loads in Hypersonic Aeroelasticity", International Forum on Aeroelasticity and Structural Dynamics, Paper 2007-099, Stockholm, June 2007.
-
(2007)
International Forum on Aeroelasticity and Structural Dynamics, Paper 2007-099
-
-
McNamara, J.J.1
Gogulapati, A.2
Friedmann, P.P.3
Banavara, N.K.4
-
40
-
-
72549108577
-
Supersonic flutter analysis based on local piston theory
-
Oct, doi:10.2514/1.37750
-
Zhang, W. W., Ye, Z. Y., Zhang, C. A., and Liu, F., "Supersonic Flutter Analysis Based on Local Piston Theory", AIAA Journal, Vol. 47, No. 10, Oct. 2009, pp. 2321-2328. doi:10.2514/1.37750
-
(2009)
AIAA Journal
, vol.47
, Issue.10
, pp. 2321-2328
-
-
Zhang, W.W.1
Ye, Z.Y.2
Zhang, C.A.3
Liu, F.4
-
41
-
-
0004170146
-
-
1st ed., Academic Press, New York
-
Hayes, W. D., and Probstein, R. F., Hypersonic Flow Theory, 1st ed., Academic Press, New York, 1959.
-
(1959)
Hypersonic Flow Theory
-
-
Hayes, W.D.1
Probstein, R.F.2
-
42
-
-
28844485739
-
Three-dimensional aeroelastic and aerothermoelastic behavior in hypersonic flow
-
April
-
McNamara, J. J., Friedmann, P. P., Powell, K. G., Thuruthimattam, B. J., and Bartels, R. E., "Three-Dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow", AIAA Paper 2005-2175, April 2005.
-
(2005)
AIAA Paper 2005-2175
-
-
McNamara, J.J.1
Friedmann, P.P.2
Powell, K.G.3
Thuruthimattam, B.J.4
Bartels, R.E.5
-
43
-
-
79251477013
-
Analysis of supersonic-hypersonic flutter of lifting surfaces at angle of attack
-
April
-
Yates, E., and Bennett, R., "Analysis of Supersonic-Hypersonic Flutter of Lifting Surfaces at Angle of Attack", AIAA Paper 1971-327, April 1971.
-
(1971)
AIAA Paper 1971-327
-
-
Yates, E.1
Bennett, R.2
-
44
-
-
85040285022
-
-
3rd ed., McGraw-Hill, New York
-
Anderson, J. D., Jr., Modern Compressible Flow with Historical Perspective, 3rd ed., McGraw-Hill, New York, 2003.
-
(2003)
Modern Compressible Flow with Historical Perspective
-
-
Anderson Jr., J.D.1
-
45
-
-
0003742683
-
-
English Universities Press, London
-
Cox, R. N., and Crabtree, L. F., Elements of Hypersonic Aerodynamics, English Universities Press, London, 1965.
-
(1965)
Elements of Hypersonic Aerodynamics
-
-
Cox, R.N.1
Crabtree, L.F.2
-
46
-
-
0003595356
-
-
NASATM 1998-208444
-
Krist, S. L., Biedron, R. T., and Rumsey, C. L., "CFL3D User's Manual (Version 5.0)", NASATM 1998-208444, 1997;
-
(1997)
CFL3D User's Manual (Version 5.0)
-
-
Krist, S.L.1
Biedron, R.T.2
Rumsey, C.L.3
-
47
-
-
79251483302
-
-
also CFL3D Version 6.4, Oct
-
also CFL3D Version 6.4, Oct. 2005.
-
(2005)
-
-
-
48
-
-
77949603890
-
-
NASA TM 2006-214301
-
Bartels, R. E., Rumsey, C. L., and Biedron, R. T., "CFL3D User's Manual-General Usage and Aeroelastic Analysis (Version 6.4)", NASA TM 2006-214301, 2006.
-
(2006)
CFL3D User's Manual-general Usage and Aeroelastic Analysis (Version 6.4)
-
-
Bartels, R.E.1
Rumsey, C.L.2
Biedron, R.T.3
-
49
-
-
34547570918
-
Flutter-boundary identification for time-domain computational aeroelasticity
-
July, doi:10.2514/1.26706
-
McNamara, J. J., and Friedmann, P. P., "Flutter-Boundary Identification for Time-Domain Computational Aeroelasticity", AIAA Journal, Vol. 45, No. 7, July 2007, pp. 1546-1555. doi:10.2514/1.26706
-
(2007)
AIAA Journal
, vol.45
, Issue.7
, pp. 1546-1555
-
-
McNamara, J.J.1
Friedmann, P.P.2
-
50
-
-
0024091975
-
Modern wing flutter analysis by computational fluid dynamic methods
-
doi:10.2514/3.45686
-
Cunningham, H. J., Batina, J. T., and Bennett, R. M., "Modern Wing Flutter Analysis by Computational Fluid Dynamic Methods", Journal of Aircraft, Vol. 25, No. 10, 1988, pp. 962-968. doi:10.2514/3.45686
-
(1988)
Journal of Aircraft
, vol.25
, Issue.10
, pp. 962-968
-
-
Cunningham, H.J.1
Batina, J.T.2
Bennett, R.M.3
-
51
-
-
0026261105
-
Aeroelastic analysis of wings using the euler equations with a deforming mesh
-
Nov, doi:10.2514/3.46096
-
Robinson, B. A., Batina, J. T., and Yang, H. T., "Aeroelastic Analysis of Wings Using the Euler Equations with a Deforming Mesh", Journal of Aircraft, Vol. 28, No. 11, Nov. 1991, pp. 781-788. doi:10.2514/3.46096
-
(1991)
Journal of Aircraft
, vol.28
, Issue.11
, pp. 781-788
-
-
Robinson, B.A.1
Batina, J.T.2
Yang, H.T.3
-
52
-
-
5244381682
-
New time domain technique for flutter boundary identification
-
April
-
Pak, C. G., and Friedmann, P. P., "New Time Domain Technique for Flutter Boundary Identification", AIAA Paper 1992-2102, April 1992.
-
(1992)
AIAA Paper 1992-2102
-
-
Pak, C.G.1
Friedmann, P.P.2
-
53
-
-
0035082795
-
Flutter margin evaluation for discrete-time systems
-
Jan.-Feb, doi:10.2514/2.2732
-
Torii, H., and Matsuzaki, Y., "Flutter Margin Evaluation for Discrete-Time Systems", Journal of Aircraft, Vol. 38, No. 1, Jan.-Feb. 2001, pp. 42-47. doi:10.2514/2.2732
-
(2001)
Journal of Aircraft
, vol.38
, Issue.1
, pp. 42-47
-
-
Torii, H.1
Matsuzaki, Y.2
-
54
-
-
34547563599
-
Aeroelastic and aerothermoelastic analysis of hypersonic vehicles: Current status and future trends
-
April
-
McNamara, J. J., and Friedmann, P. P., "Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends", AIAA Paper 2007-2013, April 2007.
-
(2007)
AIAA Paper 2007-2013
-
-
McNamara, J.J.1
Friedmann, P.P.2
-
55
-
-
0027628154
-
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
-
July-Aug, doi:10.2514/3.56890
-
Heeg, J., Gilbert, M. G., and Pototzky, A. S., "Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft", Journal of Aircraft, Vol. 30, No. 4, July-Aug. 1993, pp. 453-458. doi:10.2514/3.56890
-
(1993)
Journal of Aircraft
, vol.30
, Issue.4
, pp. 453-458
-
-
Heeg, J.1
Gilbert, M.G.2
Pototzky, A.S.3
-
56
-
-
84972517827
-
Design and analysis of computer experiments
-
doi:10.1214/ss/1177012413
-
Sacks, J., Welch, W. J., Mitchell, T. J., and Wynn, H. P., "Design and Analysis of Computer Experiments", Statistical Science, Vol. 4, No. 4, 1989, pp. 409-435. doi:10.1214/ss/1177012413
-
(1989)
Statistical Science
, vol.4
, Issue.4
, pp. 409-435
-
-
Sacks, J.1
Welch, W.J.2
Mitchell, T.J.3
Wynn, H.P.4
-
57
-
-
0035659213
-
Kriging models for global approximation in simulation-based multidisciplinary design optimization
-
Dec, doi:10.2514/2.1234
-
Simpson, T. W., Mauery, T. M., Korte, J. J., and Mistree, F., "Kriging Models for Global Approximation in Simulation-Based Multidisciplinary Design Optimization", AIAA Journal, Vol. 39, No. 12, Dec. 2001, pp. 2233-2241. doi:10.2514/2.1234
-
(2001)
AIAA Journal
, vol.39
, Issue.12
, pp. 2233-2241
-
-
Simpson, T.W.1
Mauery, T.M.2
Korte, J.J.3
Mistree, F.4
-
58
-
-
79251514431
-
Comparison of approximation models with merit functions for design optimization
-
Sept
-
Chung, H. S., and Alonso, J. J., "Comparison of Approximation Models with Merit Functions for Design Optimization", AIAA Paper 2000-4754, Sept. 2000.
-
(2000)
AIAA Paper 2000-4754
-
-
Chung, H.S.1
Alonso, J.J.2
-
59
-
-
10444244236
-
DACE A MATLAB kriging toolbox version 2.0
-
Lophaven, S. N., Nielsen, H. B., and Sondergaard, J., "DACE A MATLAB Kriging Toolbox Version 2.0", IMM Technical Report TR-2002-12, 2002.
-
(2002)
IMM Technical Report TR-2002-12
-
-
Lophaven, S.N.1
Nielsen, H.B.2
Sondergaard, J.3
-
60
-
-
77958591004
-
Reduced order aerothermodynamics for two-way coupled aerothermoelasticity in hypersonic flow
-
Seattle, WA, June
-
Crowell, A. R., Culler, A. J., and McNamara, J. J., "Reduced Order Aerothermodynamics for Two-way Coupled Aerothermoelasticity in Hypersonic Flow", International ForumonAeroelasticity and Structural Dynamics, Paper 2009-094, Seattle, WA, June 2009.
-
(2009)
International ForumonAeroelasticity and Structural Dynamics, Paper 2009-094
-
-
Crowell, A.R.1
Culler, A.J.2
McNamara, J.J.3
-
61
-
-
79961098678
-
Determinationof the optimal set of parameters of a kriging model for an euler based induced drag function
-
Seattle, WA, June
-
Kolonay, R. M., and Lambe, L. A., "Determinationof the Optimal Set of Parameters of a Kriging Model for an Euler Based Induced Drag Function", International Forum on Aeroelasticity and Structural Dynamics, Paper 2009-005, Seattle, WA, June 2009.
-
(2009)
International Forum on Aeroelasticity and Structural Dynamics, Paper 2009-005
-
-
Kolonay, R.M.1
Lambe, L.A.2
-
62
-
-
34250804357
-
Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model
-
Jan
-
Kumano, T., Jeong, S., Obayashi, S., Ito, Y., Hatanaka, K., and Morino, H., "Multidisciplinary Design Optimization of Wing Shape for a Small Jet Aircraft Using Kriging Model", AIAA Paper 2006-932, Jan. 2006.
-
(2006)
AIAA Paper 2006-932
-
-
Kumano, T.1
Jeong, S.2
Obayashi, S.3
Ito, Y.4
Hatanaka, K.5
Morino, H.6
-
63
-
-
70349586798
-
Coupled aerostructural design optimization using the kriging model and integrated multiobjective optimization algorithm
-
Sept, doi:10.1007/s10957-009-9520-9
-
Lam, X. B., Kim, Y. S., Hoang, A. D., and Park, C. W., "Coupled Aerostructural Design Optimization Using the Kriging Model and Integrated Multiobjective Optimization Algorithm", Journal of Optimization Theory and Applications, Vol. 142, No. 3, Sept. 2009, pp. 533-556. doi:10.1007/s10957-009- 9520-9
-
(2009)
Journal of Optimization Theory and Applications
, vol.142
, Issue.3
, pp. 533-556
-
-
Lam, X.B.1
Kim, Y.S.2
Hoang, A.D.3
Park, C.W.4
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