-
1
-
-
0021515347
-
Slender Wings with Leading- Edge Vortex Separation: A Challenge for Panel Methods and Euler Solvers
-
Hitzel, S. M., and Schmidt, W., “Slender Wings with Leading- Edge Vortex Separation: A Challenge for Panel Methods and Euler Solvers,” Journal of Aircraft, Vol. 21, No. 10, 1984, pp. 751-759.
-
(1984)
Journal of Aircraft
, vol.21
, Issue.10
, pp. 751-759
-
-
Hitzel, S.M.1
Schmidt, W.2
-
2
-
-
0021522778
-
Computation of Flow around Wings Based on the Euler Equations
-
Rizzi, A. W., and Eriksson, L. E., “Computation of Flow around Wings Based on the Euler Equations,” Journal of Fluid Mechanics, Vol. 148, 1984, pp. 45-71.
-
(1984)
Journal of Fluid Mechanics
, vol.148
, pp. 45-71
-
-
Rizzi, A.W.1
Eriksson, L.E.2
-
3
-
-
85003412120
-
Methode de calcul d'ecoulements autour de missiles tactiques a 1'aide d'un schema decentre, (Calculation Method for the Flow past Tactical Missiles with a Non-Centered Scheme)
-
French and English editions
-
Borrel, M., Montagne, J.-L., Diet, J., Guillen, Ph., and Lordon, J., “Methode de calcul d'ecoulements autour de missiles tactiques a 1'aide d'un schema decentre,” (Calculation Method for the Flow past Tactical Missiles with a Non-Centered Scheme), La Recherche Aerospatiale, French and English editions, No. 2, 1988, pp. 43-55.
-
(1988)
La Recherche Aerospatiale
, vol.2
, pp. 43-55
-
-
Borrel, M.1
Montagne, J.-L.2
Diet, J.3
Guillen, P.H.4
Lordon, J.5
-
4
-
-
0025249397
-
Hybrid Finite Volume Approach to Euler Solutions for Supersonic Flows
-
Siclari, M. J., and Del Guidice, P., “Hybrid Finite Volume Approach to Euler Solutions for Supersonic Flows,” AIAA Journal, Vol. 28, No. 1, 1990, pp. 66-74.
-
(1990)
AIAA Journal
, vol.28
, Issue.1
, pp. 66-74
-
-
Siclari, M.J.1
Del Guidice, P.2
-
5
-
-
84997612750
-
-
AGARD CP 493
-
Lordon, J., Fare, J. C., and Pagan, D., “Supersonic Vortex Flows around a Missile Body. Basic Experiment and Euler Numerical Modelisation,” AGARD CP 493, 1990.
-
(1990)
Supersonic Vortex Flows around a Missile Body. Basic Experiment and Euler Numerical Modelisation
-
-
Lordon, J.1
Fare, J.C.2
Pagan, D.3
-
6
-
-
84889184566
-
-
AGARD CP 412
-
Kordulla, W., Vollmers, H., and Dallmann, U., “Simulation of Three-Dimensional Transonic Flow with Separation past a Hemisphere- Cylinder Configuration,” AGARD CP 412, 1986.
-
(1986)
Simulation of Three-Dimensional Transonic Flow with Separation past a Hemisphere- Cylinder Configuration
-
-
Kordulla, W.1
Vollmers, H.2
Dallmann, U.3
-
7
-
-
85003319869
-
-
National Aerospace Lab., The Netherlands, MP-84078U, Stockholm, Sweden, Oct. 1-3
-
Elsenaar, A., and Eriksson, G., Proceedings of the Symposium on the International Vortex Flow Experiment on Euler Code Validation, National Aerospace Lab., The Netherlands, MP-84078U, Stockholm, Sweden, Oct. 1-3, 1986.
-
(1986)
Proceedings of the Symposium on the International Vortex Flow Experiment on Euler Code Validation
-
-
Elsenaar, A.1
Eriksson, G.2
-
8
-
-
0022664022
-
Numerical Simulation of Leading Edge Vortex Flows
-
Rizzetta, D. P., and Shang, J. S., “Numerical Simulation of Leading Edge Vortex Flows,” AIAA Journal, Vol. 24, No. 2, 1986, pp. 237-245.
-
(1986)
AIAA Journal
, vol.24
, Issue.2
, pp. 237-245
-
-
Rizzetta, D.P.1
Shang, J.S.2
-
9
-
-
0024732381
-
Numerical Simulation of Vortical Flows over a Strake-Delta Wing
-
Fuji, K., and Schiff, L. B., “Numerical Simulation of Vortical Flows over a Strake-Delta Wing,” AIAA Journal, Vol. 27, No. 9, 1989, pp. 1153-1162.
-
(1989)
AIAA Journal
, vol.27
, Issue.9
, pp. 1153-1162
-
-
Fuji, K.1
Schiff, L.B.2
-
10
-
-
0024732107
-
Computational Analysis of Three-Dimensional Turbulent Flow around a Bluff Body in Ground Proximity
-
Han, T., “Computational Analysis of Three-Dimensional Turbulent Flow around a Bluff Body in Ground Proximity,” AIAA Journal, Vol. 27, No. 9, 1989, pp. 1213-1219.
-
(1989)
AIAA Journal
, vol.27
, Issue.9
, pp. 1213-1219
-
-
Han, T.1
-
11
-
-
0024922962
-
Navier-Stokes Computations of Lee-Side Flows over Delta Wings
-
Thomas, J. L., and Newsome, R. W., “Navier-Stokes Computations of Lee-Side Flows over Delta Wings,” AIAA Journal, Vol. 27, No. 12, 1989, pp. 1673-1679.
-
(1989)
AIAA Journal
, vol.27
, Issue.12
, pp. 1673-1679
-
-
Thomas, J.L.1
Newsome, R.W.2
-
12
-
-
0024765109
-
Topology of the Flow Structures Behind an Inclined Projectile: Parts A and B
-
Ward, K. C., and Katz, J., “Topology of the Flow Structures Behind an Inclined Projectile: Parts A and B,” Journal of Aircraft, Vol. 26, No. 11, 1989, pp. 1016-1031.
-
(1989)
Journal of Aircraft
, vol.26
, Issue.11
, pp. 1016-1031
-
-
Ward, K.C.1
Katz, J.2
-
13
-
-
0025431519
-
Numerical Analysis of Three- Dimensional Viscous Internal Flows
-
Chima, R. V., and Yokota, J. W., “Numerical Analysis of Three- Dimensional Viscous Internal Flows,” AIAA Journal, Vol. 28, No. 5, 1990, pp. 798-806.
-
(1990)
AIAA Journal
, vol.28
, Issue.5
, pp. 798-806
-
-
Chima, R.V.1
Yokota, J.W.2
-
14
-
-
0025446832
-
Navier-Stokes Computation of Flow around a Round-Edge Double-Delta Wing
-
Hsu, C. H., and Liu, C. H., “Navier-Stokes Computation of Flow around a Round-Edge Double-Delta Wing,” AIAA Journal, Vol. 28, No. 6, 1990, pp. 961-970.
-
(1990)
AIAA Journal
, vol.28
, Issue.6
, pp. 961-970
-
-
Hsu, C.H.1
Liu, C.H.2
-
15
-
-
0025462326
-
Navier-Stokes Solutions for Vortical Flows over a Tangent-Ogive Cylinder
-
Hartwich, P. M., and Hall, R. M., “Navier-Stokes Solutions for Vortical Flows over a Tangent-Ogive Cylinder,” AIAA Journal, Vol. 28, No. 7, 1990, pp. 1171-1179.
-
(1990)
AIAA Journal
, vol.28
, Issue.7
, pp. 1171-1179
-
-
Hartwich, P.M.1
Hall, R.M.2
-
16
-
-
0002297003
-
Ecoulement au voisinage de la pointe avant d'une aile a forte fleche aux incidences moyennes, (Flow in the Vicinity of the Apex of a Wing with Large Sweep Angle at Moderate Incidences)
-
Legendre, R., “Ecoulement au voisinage de la pointe avant d'une aile a forte fleche aux incidences moyennes,” (Flow in the Vicinity of the Apex of a Wing with Large Sweep Angle at Moderate Incidences), La Recherche Aeronautique, No. 30, 1952, pp. 3-8.
-
(1952)
La Recherche Aeronautique
, vol.30
, pp. 3-8
-
-
Legendre, R.1
-
17
-
-
0002297003
-
Separation de 1'ecoulement laminaire tridimensionnel, (Separation of a Laminar Three-Dimensional Flow)
-
Legendre, R., “Separation de 1'ecoulement laminaire tridimensionnel,” (Separation of a Laminar Three-Dimensional Flow), La Recherche Aeronautique, No. 54, 1956, pp. 3-8.
-
(1956)
La Recherche Aeronautique
, vol.54
, pp. 3-8
-
-
Legendre, R.1
-
18
-
-
0010282441
-
Lignes de courant d'un ecoulement permanent. Decollement et separation (Streamlines of a Steady Flow. Separation and Separators)
-
Legendre, R., “Lignes de courant d'un ecoulement permanent. Decollement et separation” (Streamlines of a Steady Flow. Separation and Separators), La Recherche Aerospatiale, No. 6, 1977, pp. 327-335.
-
(1977)
La Recherche Aerospatiale
, vol.6
, pp. 327-335
-
-
Legendre, R.1
-
19
-
-
0042957491
-
-
edited by H. Gortler, Springer-Verlag, Berlin
-
Oswatitsch, K., “Die Ablosungsbedingung von Grenzschichten,” Grenzschichtforschung, edited by H. Gortler, Springer-Verlag, Berlin, 1958, pp. 357-367.
-
(1958)
Die Ablosungsbedingung Von Grenzschichten, Grenzschichtforschung
, pp. 357-367
-
-
Oswatitsch, K.1
-
20
-
-
85002611768
-
Attachment and Separation in Three-Dimensional Flow
-
edited by L. Rosenhead, Oxford University Press, Oxford, England, UK, Sec. II, Chaps. 2-6
-
Lighthill, J. M., “Attachment and Separation in Three-Dimensional Flow,” Laminar Boundary-Layer Theory, edited by L. Rosenhead, Oxford University Press, Oxford, England, UK, Sec. II, Chaps. 2-6, pp. 72-82.
-
Laminar Boundary-Layer Theory
, pp. 72-82
-
-
Lighthill, J.M.1
-
21
-
-
85003335139
-
-
Ph.D. Dissertation, Univ. Claude Bernard, Lyon, France, Sept
-
Chanetz, B., “Contribution a 1'etude du decollement tridimensionnel en ecoulement turbulent incompressible,” (Contribution to the Study of Three-Dimensional Separation in Incompressible Turbulent Flow), Ph.D. Dissertation, Univ. Claude Bernard, Lyon, France, Sept. 1986.
-
(1986)
Contribution a 1'Etude Du Decollement Tridimensionnel En Ecoulement Turbulent incompressible,” (Contribution to the Study of Three-Dimensional Separation in Incompressible Turbulent Flow)
-
-
Chanetz, B.1
-
22
-
-
77957067853
-
Critical Points in Flow Patterns
-
Perry, A. E., and Fairlie, B. D., “Critical Points in Flow Patterns,” Advance in Geophysics, Vol. B-18, 1974, pp. 299-315.
-
(1974)
Advance in Geophysics
, vol.B-18
, pp. 299-315
-
-
Perry, A.E.1
Fairlie, B.D.2
-
23
-
-
0346394752
-
Boundary-Layer over a Blunt Body at Low Incidence with Circumferential Reversed Flow
-
Wang, K. C., “Boundary-Layer over a Blunt Body at Low Incidence with Circumferential Reversed Flow,” Journal of Fluid Mechanics, Vol. 72, Part I, 1975, pp. 49-65.
-
(1975)
Journal of Fluid Mechanics
, vol.72
, pp. 49-65
-
-
Wang, K.C.1
-
24
-
-
0019939104
-
Topology of Three-Dimensional Separated Flows
-
Tobak, M., and Peake, D. J., “Topology of Three-Dimensional Separated Flows,” Annual Review of Fluid Mechanics, Vol. 14,1982, pp. 61-85.
-
(1982)
Annual Review of Fluid Mechanics
, vol.14
, pp. 61-85
-
-
Tobak, M.1
Peake, D.J.2
-
26
-
-
0021394013
-
Some Aspects of Three-Dimensional Separation. Part I: Streamsurface Bifurcations
-
Hornung, H., and Perry, A. E., “Some Aspects of Three-Dimensional Separation. Part I: Streamsurface Bifurcations,” Zeitschrift fur Flugwiss. Weltraumforsch. 8, Heft, 2, 1984, pp. 77-87.
-
(1984)
Zeitschrift Fur Flugwiss. Weltraumforsch.
, vol.8
, Issue.2
, pp. 77-87
-
-
Hornung, H.1
Perry, A.E.2
-
27
-
-
0023242925
-
A Description of Eddying Motions and Flow Patterns Using Critical Point Concepts
-
Perry, A. E., and Chong, M. S., “A Description of Eddying Motions and Flow Patterns Using Critical Point Concepts,” Annual Review of Fluid Mechanics, Vol. 19, 1987, pp. 125-155.
-
(1987)
Annual Review of Fluid Mechanics
, vol.19
, pp. 125-155
-
-
Perry, A.E.1
Chong, M.S.2
-
28
-
-
85003283376
-
-
AIAA Paper 86-0508, Reno, NV, Jan
-
Kaynak, U., Cantwell, B. J., Hoist, T. L., and Sorensen, R. L., “Numerical Simulation of Transonic Separated Flows over Low Aspect Ratio Wings,” AIAA Paper 86-0508, Reno, NV, Jan. 1986.
-
(1986)
Numerical Simulation of Transonic Separated Flows over Low Aspect Ratio Wings
-
-
Kaynak, U.1
Cantwell, B.J.2
Hoist, T.L.3
Sorensen, R.L.4
-
30
-
-
0024732382
-
Reynolds Number Effect on Separation Structures at Normal Shock Wave/Turbulent Boundary Layer Interaction
-
Doerffer, P., and Dallmann, U., “Reynolds Number Effect on Separation Structures at Normal Shock Wave/Turbulent Boundary Layer Interaction,” AIAA Journal, Vol. 27, No. 9, 1989, pp. 1206- 1212.
-
(1989)
AIAA Journal
, vol.27
, Issue.9
-
-
Doerffer, P.1
Dallmann, U.2
-
31
-
-
85003348481
-
-
AIAA Paper 89- 0353, Reno, NV, Jan
-
Doerffer, P., and Dallmann, U., “Mach Number Dependence of Flow Separation-Induced by Normal Shock Wave/Turbulent Boundary Layer Interaction at a Curved Wall,” AIAA Paper 89- 0353, Reno, NV, Jan. 1989.
-
(1989)
Mach Number Dependence of Flow Separation-Induced by Normal Shock Wave/Turbulent Boundary Layer Interaction at a Curved Wall
-
-
Doerffer, P.1
Dallmann, U.2
-
32
-
-
85002562587
-
Evolution reguliere ou catastrophique d'ecoulements permanents dependant de parametres
-
Legendre, R., “Evolution reguliere ou catastrophique d'ecoulements permanents dependant de parametres,” La Recherche Aerospatiale, No. 4, 1982, pp. 225-232.
-
(1982)
La Recherche Aerospatiale
, Issue.4
, pp. 225-232
-
-
Legendre, R.1
-
33
-
-
0007664303
-
-
AIAA Paper 86-0485, Reno, NV, Jan
-
Chapman, G. T., “Topological Classification of Flow Separation on Three-Dimensional Bodies,” AIAA Paper 86-0485, Reno, NV, Jan. 1986.
-
(1986)
Topological Classification of Flow Separation on Three-Dimensional Bodies
-
-
Chapman, G.T.1
-
35
-
-
0021428983
-
Some Aspects of Three-Dimensional Separation. Part II: Vortex Skeleton
-
Perry, A. E., and Hornung, H., “Some Aspects of Three-Dimensional Separation. Part II: Vortex Skeleton,” Zeitschrift fur Flugwiss. Weltraumforsch. 8, Heft 3, 1984, pp. 155-160.
-
(1984)
Zeitschrift Fur Flugwiss. Weltraumforsch.
, vol.8
, Issue.3
, pp. 155-160
-
-
Perry, A.E.1
Hornung, H.2
-
38
-
-
85006741798
-
-
AIAA Paper 91-1713, June
-
Hung, C. M., Sung, C. H., and Chen, C. L., “Computation of Saddle Point of Attachment,” AIAA Paper 91-1713, June 1991.
-
(1991)
Computation of Saddle Point of Attachment
-
-
Hung, C.M.1
Sung, C.H.2
Chen, C.L.3
-
40
-
-
0018479027
-
A Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
-
Settles, G. S., Fitzpatrick, T. J., and Bogdonoff, S. M., “A Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow,” AIAA Journal, Vol. 17, No. 6, 1979, pp. 579-585.
-
(1979)
AIAA Journal
, vol.17
, Issue.6
, pp. 579-585
-
-
Settles, G.S.1
Fitzpatrick, T.J.2
Bogdonoff, S.M.3
-
41
-
-
85003365646
-
Observations of Turbulent Reattachment behind an Axisymmetric Downstream Facing Step in Supersonic Flow
-
Roshko, A., and Thomke, G. J., “Observations of Turbulent Reattachment behind an Axisymmetric Downstream Facing Step in Supersonic Flow,” AIAA Journal, Vol. 4, No. 6, 1966, pp. 975-980.
-
(1966)
AIAA Journal
, vol.4
, Issue.6
, pp. 975-980
-
-
Roshko, A.1
Thomke, G.J.2
-
42
-
-
85003403241
-
-
private communication
-
Joulot, A., private communication, 1990.
-
(1990)
-
-
Joulot, A.1
-
43
-
-
0017465751
-
Three-Dimensional Heat and Mass Transfer Effects across High-Speed Reattaching Flows
-
Inger, G. R., “Three-Dimensional Heat and Mass Transfer Effects across High-Speed Reattaching Flows,” AIAA Journal, Vol. 15, No. 3, 1977, pp. 383-389.
-
(1977)
AIAA Journal
, vol.15
, Issue.3
, pp. 383-389
-
-
Inger, G.R.1
-
46
-
-
85007106972
-
-
AIAA Paper 89-1851, Buffalo, New York, June
-
Cambier, L., and Escande, B., “Navier-Stokes Simulation of a Shock Wave/Turbulent Boundary Layer Interaction in a Three-Dimensional Channel.” AIAA Paper 89-1851, Buffalo, New York, June 1989
-
(1989)
Navier-Stokes Simulation of a Shock Wave/Turbulent Boundary Layer Interaction in a Three-Dimensional Channel.
-
-
Cambier, L.1
Escande, B.2
-
47
-
-
85003272689
-
-
AIAA Journal, Vol. 28, No. 11,1990, pp. 1901-1908.
-
(1990)
AIAA Journal
, vol.28
, Issue.11
, pp. 1901-1908
-
-
-
48
-
-
0003057517
-
Analyse experimentale de I'ecoulement dans un canal transsonique tridimensionnel (Experimental Analysis of the Flow in a Three-Dimensional Transonic Channel)
-
French and English editions
-
Benay, R., Delery, J., and Pot, T., “Analyse experimentale de I'ecoulement dans un canal transsonique tridimensionnel” (Experimental Analysis of the Flow in a Three-Dimensional Transonic Channel), La Recherche Aerospatiale, French and English editions, No. 6, 1986, pp. 399-414.
-
(1986)
La Recherche Aerospatiale
, Issue.6
, pp. 399-414
-
-
Benay, R.1
Delery, J.2
Pot, T.3
-
49
-
-
49849110318
-
Interactions Between Shock Waves and Turbulent Boundary Layers
-
edited by D. Kiichemann et al., Vol. II, Pergamon, Oxford
-
Green, J. E., “Interactions Between Shock Waves and Turbulent Boundary Layers,” Progress in Aerospace Sciences, edited by D. Kiichemann et al., Vol. II, Pergamon, Oxford, 1970.
-
(1970)
Progress in Aerospace Sciences
-
-
Green, J.E.1
-
50
-
-
0015588288
-
-
AIAA Paper 72- 715, Boston, MA, ;see also, AIAA Journal, Vol 11, No. 2,1973, pp. 139-140
-
Reda, D. C., and Murthy, J. D., “Shock Wave/Turbulent Boundary Layer Interactions in Rectangular Channels,” AIAA Paper 72- 715, Boston, MA, 1972; see also, AIAA Journal, Vol 11, No. 2,1973, pp. 139-140.
-
(1972)
Shock Wave/Turbulent Boundary Layer Interactions in Rectangular Channels
-
-
Reda, D.C.1
Murthy, J.D.2
-
51
-
-
0022062316
-
Turbulent Boundary Layer Development in an Adverse Pressure Gradient after an Interaction with a Normal Shock Wave
-
Schofield, W. H., “Turbulent Boundary Layer Development in an Adverse Pressure Gradient after an Interaction with a Normal Shock Wave,” Journal of Fluid Mechanics, Vol. 154, 1985, pp. 43- 62.
-
(1985)
Journal of Fluid Mechanics
, vol.154
-
-
Schofield, W.H.1
-
52
-
-
0007948670
-
-
AIAA Paper 87-1266, Honolulu, HI, June
-
Dallmann, U., and Schewe, G. “On Topological Changes of Separating Flow Structures at Transition Reynolds Numbers,” AIAA Paper 87-1266, Honolulu, HI, June 1987.
-
(1987)
On Topological Changes of Separating Flow Structures at Transition Reynolds Numbers
-
-
Dallmann, U.1
Schewe, G.2
-
55
-
-
0020824710
-
Vortex Flow over Delta and Double-Delta Wings
-
Hoeijmakers, H. W. M., Vaatstra, W., and Verhaagen, N. G., “Vortex Flow over Delta and Double-Delta Wings,” Journal of Aircraft, Vol. 20, No. 9, 1983, pp. 825-832.
-
(1983)
Journal of Aircraft
, vol.20
, Issue.9
, pp. 825-832
-
-
Hoeijmakers, H.W.M.1
Vaatstra, W.2
Verhaagen, N.G.3
-
56
-
-
85003409194
-
-
AIAA Paper 87- 2425, Aug
-
Taylor, S. L., Kjelgaard, S. O., Weston, R. P., Thomas, J. L., and Sellers, W. L., “Experimental and Computational Study of the Subsonic Flow about a 75° Swept Delta-Wing,” AIAA Paper 87- 2425, Aug. 1987.
-
(1987)
Experimental and Computational Study of the Subsonic Flow about a 75° Swept Delta-Wing
-
-
Taylor, S.L.1
Kjelgaard, S.O.2
Weston, R.P.3
Thomas, J.L.4
Sellers, W.L.5
-
57
-
-
78149463775
-
Experimental Study on Vortex and Shock Wave Development on a 65° Delta Wing
-
edited by J. Zierep and H. Oertels, Springer- Verlag, Berlin
-
Elsenaar, A., and Butefisch, K. A., “Experimental Study on Vortex and Shock Wave Development on a 65° Delta Wing,” Symposium Transsonicum III, edited by J. Zierep and H. Oertels, Springer- Verlag, Berlin, 1988.
-
(1988)
Symposium Transsonicum III
-
-
Elsenaar, A.1
Butefisch, K.A.2
-
59
-
-
3342896211
-
-
AIAA Paper 90- 0599, Reno, NV, Jan
-
Kegelman, J. T., and Roos, F. W., “The Flowfields of Bursting Vortices Over Moderately Swept Delta Wings,” AIAA Paper 90- 0599, Reno, NV, Jan. 1990.
-
(1990)
The Flowfields of Bursting Vortices over Moderately Swept Delta Wings
-
-
Kegelman, J.T.1
Roos, F.W.2
-
62
-
-
85003244746
-
Etude experimentale de I'ecoulement a 1'extrados d'une aile delta en regime incompressible” (Experimental Study of the Flow on the Suction Side of a Delta Wing in Incompressible Flow)
-
French and English editions
-
Solignac, J.-L., Pagan, D., and Molton, P., “Etude experimentale de I'ecoulement a 1'extrados d'une aile delta en regime incompressible” (Experimental Study of the Flow on the Suction Side of a Delta Wing in Incompressible Flow), La Recherche Aerospatiale, French and English editions, No. 6, 1989, pp. 47-65.
-
(1989)
La Recherche Aerospatiale
, Issue.6
, pp. 47-65
-
-
Solignac, J.-L.1
Pagan, D.2
Molton, P.3
-
63
-
-
85003310605
-
-
AGARD CP 30
-
Monnerie, B., and Werle, H., “Etude de 1'ecoulement supersonique et hypersonique autour d'une aile elancee en fleche” (Study of the Supersonic and Hypersonic Flow Past a Slender, Highly Swept Wing), AGARD CP 30, 1968.
-
(1968)
Etude De 1'Ecoulement Supersonique Et Hypersonique Autour D'une Aile Elancee En Fleche (Study of the Supersonic and Hypersonic Flow past a Slender, Highly Swept Wing)
-
-
Monnerie, B.1
Werle, H.2
-
65
-
-
84889537551
-
Measurements and Interpretation of 3-D High Speed Flows
-
Swansea, Wales, UK, Sept. 26-29, and French- German Inst. of Saint-Louis, Rept. CO 242/89
-
Berner, C., “Measurements and Interpretation of 3-D High Speed Flows,” Proceedings of the Third International Conference on Laser Anemometry, Swansea, Wales, UK, Sept. 26-29, 1989 and French- German Inst. of Saint-Louis, Rept. CO 242/89.
-
(1989)
Proceedings of the Third International Conference on Laser Anemometry
-
-
Berner, C.1
-
66
-
-
85003261776
-
-
French-German Inst. of Saint- Louis, Rept. S-CR 2/90
-
Berner, C., and Duperoux, J. P., “Mesures simultanees des trois composantes du vecteur vitesse dans le sillage d'arriere-corps a symetrie de revolution et en incidence” (Simultaneous Measurements of the Velocity Vector Three Components in the Wake of an Axisymmetric Afterbody at an Incidence), French-German Inst. of Saint- Louis, Rept. S-CR 2/90, 1990.
-
(1990)
Mesures Simultanees Des Trois Composantes Du Vecteur Vitesse Dans Le Sillage D'arriere-Corps a Symetrie De Revolution Et En incidence” (Simultaneous Measurements of the Velocity Vector Three Components in the Wake of an Axisymmetric Afterbody at an Incidence
-
-
Berner, C.1
Duperoux, J.P.2
-
68
-
-
0017725767
-
Investigation of Slender-Body Vortices
-
Dec
-
Fidler, J. E., Schwind, R. G., and Nielsen, J. N., “Investigation of Slender-Body Vortices,” AIAA Journal, Vol. 15, No. 12, Dec. 1977, pp. 1736-1741.
-
(1977)
AIAA Journal
, vol.15
, Issue.12
, pp. 1736-1741
-
-
Fidler, J.E.1
Schwind, R.G.2
Nielsen, J.N.3
-
69
-
-
85003300021
-
Flowfield about and Forces on Slender Bodies at High Angles of Attack
-
Yanta, W. J., and Wardlaw, A. B., Jr., “Flowfield about and Forces on Slender Bodies at High Angles of Attack,” AIAA Journal, Vol. 19, No. 3, 1981, pp. 296-302.
-
(1981)
AIAA Journal
, vol.19
, Issue.3
, pp. 296-302
-
-
Yanta, W.J.1
Wardlaw, A.B.2
-
70
-
-
0019913017
-
-
AIAA Paper 82-0343, Orlando, FL, Jan
-
Yanta, W. J., and Wardlaw, A. B., Jr., “The Secondary Separation Region on a Body at High Angles of Attack,” AIAA Paper 82-0343, Orlando, FL, Jan. 1982.
-
(1982)
The Secondary Separation Region on a Body at High Angles of Attack
-
-
Yanta, W.J.1
Wardlaw, A.B.2
-
71
-
-
85003369019
-
The Analysis and Modelling of Body Vortex Flowfields around Missile Configurations and their Interaction with Lifting Surfaces at Subsonic and Supersonic Speeds
-
Royal Aeronautical Society, Paper 26
-
Ponton, A. J. C., and Johnson, G. A., “The Analysis and Modelling of Body Vortex Flowfields around Missile Configurations and their Interaction with Lifting Surfaces at Subsonic and Supersonic Speeds,” The Prediction and Exploitation of Separated Flows, Royal Aeronautical Society, Paper 26, 1989.
-
(1989)
The Prediction and Exploitation of Separated Flows
-
-
Ponton, A.J.C.1
Johnson, G.A.2
-
73
-
-
85003347489
-
-
), ONERA Rept. 40/ 1147AY, Jan
-
Pagan, D., and Molton, P., “Etude experimentale du systeme tourbillonnaire engendre par un fuselage de missile en incidence. Premiere partie: couche limite laminaire” (Experimental Study of the Vortex System Generated by a Missile Fuselage at an Angle of Incidence. First Part: Laminar Boundary Layer), ONERA Rept. 40/ 1147AY, Jan. 1990.
-
(1990)
Etude Experimentale Du Systeme Tourbillonnaire Engendre Par Un Fuselage De Missile En Incidence. Premiere Partie: Couche Limite laminaire” (Experimental Study of the Vortex System Generated by a Missile Fuselage at an Angle of Incidence. First Part: Laminar Boundary Layer
-
-
Pagan, D.1
Molton, P.2
-
75
-
-
0009917233
-
-
AGARD CP-342
-
Vollmers, H., Kreplin, H. P., and Meier, H. U., “Separation and Vortical-Type Flow Around a Prolate Spheroid. Evaluation of Relevant Parameters,” AGARD CP-342, 1983.
-
(1983)
Separation and Vortical-Type Flow around a Prolate Spheroid. Evaluation of Relevant Parameters
-
-
Vollmers, H.1
Kreplin, H.P.2
Meier, H.U.3
-
76
-
-
0011180542
-
-
DFVLR-IB 222-24-A11
-
Meier, H. U., Kreplin, H. P., Landhauber, A., and Baumgarten, D., “Mean Velocity Distribution in Three-Dimensional-Boundary Layers Developing on a 1:6 Prolate Spheroid with Artificial Transition,” DFVLR-IB 222-24-A11, 1984.
-
(1984)
Mean Velocity Distribution in Three-Dimensional-Boundary Layers Developing on a 1:6 Prolate Spheroid with Artificial Transition
-
-
Meier, H.U.1
Kreplin, H.P.2
Landhauber, A.3
Baumgarten, D.4
-
77
-
-
85002875690
-
-
AIAA Paper 87-1212, Honolulu, HI, June
-
Costis, C. E., Polen, D. M., Hoang, N. T., and Telionis, D. P., “Laminar Separating Flow over a Prolate Spheroid,” AIAA Paper 87-1212, Honolulu, HI, June 1987.
-
(1987)
Laminar Separating Flow over a Prolate Spheroid
-
-
Costis, C.E.1
Polen, D.M.2
Hoang, N.T.3
Telionis, D.P.4
-
78
-
-
85003467428
-
-
AIAA Paper 90-0050, Reno, NV, Jan
-
Hoang, N. T., Telionis, D. T., and Jones, G. S., “The Hemisphere- Cylinder at an Angle of Attack,” AIAA Paper 90-0050, Reno, NV, Jan. 1990.
-
(1990)
The Hemisphere- Cylinder at an Angle of Attack
-
-
Hoang, N.T.1
Telionis, D.T.2
Jones, G.S.3
-
80
-
-
84903899659
-
Etude experimentale du decollement turbulent sur un ellipsoide-cylindre aplati (Experimental Analysis of Turbulent Separation on an Oblate Ellipsoid-Cylinder)
-
French and English editions
-
Chanetz, B., and Delery, J., “Etude experimentale du decollement turbulent sur un ellipsoide-cylindre aplati” (Experimental Analysis of Turbulent Separation on an Oblate Ellipsoid-Cylinder), La Recherche Aerospatiale, French and English editions, No. 3, 1988, pp. 59-77.
-
(1988)
La Recherche Aerospatiale
, vol.3
, pp. 59-77
-
-
Chanetz, B.1
Delery, J.2
-
81
-
-
85003409108
-
Calcul de la couche limite tridimensionnelle en modes direct ou inverse sur des obstacles quelconques (Direct Mode and Inverse Mode Calculations of the Three-Dimensional Boundary Layer past Arbitrary Bodies)
-
French and English editions
-
Barberis, D., “Calcul de la couche limite tridimensionnelle en modes direct ou inverse sur des obstacles quelconques” (Direct Mode and Inverse Mode Calculations of the Three-Dimensional Boundary Layer past Arbitrary Bodies), La Recherche Aerospatiale, French and English editions, No. 3, 1986.
-
(1986)
La Recherche Aerospatiale
, Issue.3
-
-
Barberis, D.1
|