-
1
-
-
84888846131
-
Algebraic correlations for high-speed transition prediction on sharp and blunt cones
-
Kenneth K. Muramoto. Algebraic correlations for high-speed transition prediction on sharp and blunt cones. AIAA Paper No. 99-0405, 1999.
-
(1999)
AIAA Paper No. 99-0405
-
-
Muramoto, K.K.1
-
2
-
-
0014732429
-
Determination of spatial amplification factors and their application to predicting transition
-
February
-
N. A. Jaffe, T. T. Okamura, and A. M. O. Smith. "Determination of Spatial Amplification Factors and Their Application to Predicting Transition". AIAA Journal, 8(2):301-308, February 1970.
-
(1970)
AIAA Journal
, vol.8
, Issue.2
, pp. 301-308
-
-
Jaffe, N.A.1
Okamura, T.T.2
Smith, A.M.O.3
-
3
-
-
0024673637
-
Boundary-layer transition on a cone and flat plate at Mach 3.5
-
June
-
F.-J. Chen, M. R. Malik, and I. E. Beckwith. "Boundary-Layer Transition on a Cone and Flat Plate at Mach 3.5". AIAA Journal, 27:687-693, June 1989.
-
(1989)
AIAA Journal
, vol.27
, pp. 687-693
-
-
Chen, F.-J.1
Malik, M.R.2
Beckwith, I.E.3
-
4
-
-
0037485092
-
Hypersonic flight transition data analysis using parabolized stability equations with chemistry effects
-
May-June
-
Mujeeb R. Malik. "Hypersonic Flight Transition Data Analysis Using Parabolized Stability Equations with Chemistry Effects". Journal of Spacecraft and Rockets, 40(3), May-June 2003.
-
(2003)
Journal of Spacecraft and Rockets
, vol.40
, Issue.3
-
-
Malik, M.R.1
-
5
-
-
0003331444
-
Effect of nose bluntness on boundary layer stability and transition
-
January
-
M.R. Malik, R.E. Spall, and C.-L. Chang. "Effect of Nose Bluntness on Boundary Layer Stability and Transition". AIAA Paper No. 90-0112, January 1990.
-
(1990)
AIAA Paper No. 90-0112
-
-
Malik, M.R.1
Spall, R.E.2
Chang, C.-L.3
-
6
-
-
0028546374
-
Engineering transition prediction for a hypersonic axisymmetric boundary layer
-
November
-
J. Stilla. "Engineering Transition Prediction for a Hypersonic Axisymmetric Boundary Layer". AIAA Journal, 31 (6): 1358-1364, November 1994.
-
(1994)
AIAA Journal
, vol.31
, Issue.6
, pp. 1358-1364
-
-
Stilla, J.1
-
7
-
-
0006092396
-
Numerical study of hypersonic reacting boundary layer transition on cones
-
October
-
H. B. Johnson, T. G. Seipp, and G. V. Candler. "Numerical Study of Hypersonic Reacting Boundary Layer Transition on Cones". Physics of Fluids, 10(10):2676-2685, October 1998.
-
(1998)
Physics of Fluids
, vol.10
, Issue.10
, pp. 2676-2685
-
-
Johnson, H.B.1
Seipp, T.G.2
Candler, G.V.3
-
9
-
-
0032715875
-
Flight data for boundary-layer transition at hypersonic and supersonic speeds
-
Steven P. Schneider. "Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds". Journal of Spacecraft and Rockets, 36(1), 1999.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.1
-
-
Schneider, S.P.1
-
12
-
-
84997783101
-
Assessment of two-temperature kinetic model for ionizing air
-
C. Park. "Assessment of Two-Temperature Kinetic Model for Ionizing Air". AIAA Paper No. 87-1574, 1987.
-
(1987)
AIAA Paper No. 87-1574
-
-
Park, C.1
-
13
-
-
0039580351
-
Boundary-layer transition - Analysis and prediction revisited
-
January
-
Th. Herbert. "Boundary-Layer Transition - Analysis and Prediction Revisited". AIAA Paper No. 91-0737, January 1991.
-
(1991)
AIAA Paper No. 91-0737
-
-
Herbert, Th.1
-
14
-
-
0028480505
-
Oblique-mode breakdown and secondary instability in supersonic boundary layers
-
C.-L. Chang and M. R. Malik. "Oblique-mode Breakdown and Secondary Instability in Supersonic Boundary Layers". Journal of Fluid Mechanics, 273:323-359, 1994.
-
(1994)
Journal of Fluid Mechanics
, vol.273
, pp. 323-359
-
-
Chang, C.-L.1
Malik, M.R.2
-
15
-
-
0003217107
-
Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
-
Y. C. Vigneron, J. V. Rakich, and J. C. Tannehill. "Calculation of Supersonic Viscous Flow over Delta Wings with Sharp Subsonic Leading Edges". AIAA Paper No. 78-1337, 1978.
-
(1978)
AIAA Paper No. 78-1337
-
-
Vigneron, Y.C.1
Rakich, J.V.2
Tannehill, J.C.3
-
16
-
-
0024859104
-
The solution of the Navier-Stokes equations using gauss-seidel line relaxation
-
R. W. MacCormack and G. V. Candler. "The Solution of the Navier-Stokes Equations Using Gauss-Seidel Line Relaxation". Computers and Fluids, 17(1):135-150, 1989.
-
(1989)
Computers and Fluids
, vol.17
, Issue.1
, pp. 135-150
-
-
MacCormack, R.W.1
Candler, G.V.2
-
19
-
-
84964039203
-
Numerical study of hypersonic reacting boundary layer transition on cones
-
AIAA Paper No. 97-3567, June. Forthcoming in
-
H. B. Johnson, T. G. Seipp, and G. V. Candler. "Numerical Study of Hypersonic Reacting Boundary Layer Transition on Cones". AIAA Paper No. 97-3567, June 1997. Forthcoming in Physics of Fluids.
-
(1997)
Physics of Fluids
-
-
Johnson, H.B.1
Seipp, T.G.2
Candler, G.V.3
-
21
-
-
0021201692
-
Laminar boundary layer stability experiments on a cone at Mach 8, part 2: Blunt cone
-
January
-
K. F. Stetson, E. R. Thompson, J. C. Donaldson, and L. G. Siler. "Laminar Boundary Layer Stability Experiments on a Cone at Mach 8, Part 2: Blunt Cone". AIAA Paper No. 84-0006, January 1984.
-
(1984)
AIAA Paper No. 84-0006
-
-
Stetson, K.F.1
Thompson, E.R.2
Donaldson, J.C.3
Siler, L.G.4
-
26
-
-
85003342432
-
Flight test measurements of boundary layer transition on a nonablating 22° cone
-
February
-
M. M. Sherman and T. Nakamura. Flight test measurements of boundary layer transition on a nonablating 22° cone. Journal of Spacecraft and Rockets, 7(2): 137-142, February 1790.
-
(1790)
Journal of Spacecraft and Rockets
, vol.7
, Issue.2
, pp. 137-142
-
-
Sherman, M.M.1
Nakamura, T.2
|