FAR WAKE BEHIND CYLINDERS AT HYPERSONIC SPEEDS .I. FLOWFIELD

[1] VISCOUS INTERACTION EFFECTS ON A STATIC PRESSURE PROBE AT M=6 [J]. AIAA JOURNAL, 1963, 1 (12) : 2864 - 2866

[2] BEHRENS W, 1966, THESIS CALIFORNIA I

[3] MEASURED TRANSITION FROM LAMINAR TO TURBULENT FLOW AND SUBSEQUENT GROWTH OF TURBULENT WAKES [J]. AIAA JOURNAL, 1965, 3 (05) : 837 - &

[4] NEAR WAKE OF A BLUNT BODY AT HYPERSONIC SPEEDS [J]. AIAA JOURNAL, 1965, 3 (06) : 1001 - &

[5] HOT WIRE MEASUREMENTS IN LOW REYNOLDS NUMBER HYPERSONIC FLOWS [J]. ARS JOURNAL, 1961, 31 (12): : 1709 - 1718

[6] DEWEY CF, 1963, THESIS CALIFORNIA I

[7] ON TRAILS OF AXISYMMETRIC HYPERSONIC BLUNT BODIES FLYING THROUGH THE ATMOSPHERE [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (06): : 433 - &

[8] FELDMAN S, 1959, 82 AVC RES REPT

[9] LAMINAR WAKE WITH ARBITRARY INITIAL PROFILES [J]. AIAA JOURNAL, 1964, 2 (05) : 948 - 949

[10] HAYES WD, 1959, HYPERSONIC FLOW THEO, pCH9

[1] VISCOUS INTERACTION EFFECTS ON A STATIC PRESSURE PROBE AT M=6 [J]. AIAA JOURNAL, 1963, 1 (12) : 2864 - 2866

[2] BEHRENS W, 1966, THESIS CALIFORNIA I

[3] MEASURED TRANSITION FROM LAMINAR TO TURBULENT FLOW AND SUBSEQUENT GROWTH OF TURBULENT WAKES [J]. AIAA JOURNAL, 1965, 3 (05) : 837 - &

[4] NEAR WAKE OF A BLUNT BODY AT HYPERSONIC SPEEDS [J]. AIAA JOURNAL, 1965, 3 (06) : 1001 - &

[5] HOT WIRE MEASUREMENTS IN LOW REYNOLDS NUMBER HYPERSONIC FLOWS [J]. ARS JOURNAL, 1961, 31 (12): : 1709 - 1718

[6] DEWEY CF, 1963, THESIS CALIFORNIA I

[7] ON TRAILS OF AXISYMMETRIC HYPERSONIC BLUNT BODIES FLYING THROUGH THE ATMOSPHERE [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (06): : 433 - &

[8] FELDMAN S, 1959, 82 AVC RES REPT

[9] LAMINAR WAKE WITH ARBITRARY INITIAL PROFILES [J]. AIAA JOURNAL, 1964, 2 (05) : 948 - 949

[10] HAYES WD, 1959, HYPERSONIC FLOW THEO, pCH9