-
11
-
-
84915463205
-
-
M, M = 4.25).
-
-
-
-
15
-
-
84915463203
-
Subsonic static characteristics of slender wind configurations using a magnetic suspension and balance system
-
(1971)
NASA CR-1796
-
-
Vlajinac1
-
16
-
-
0015097574
-
Transition regime sphere drag near the free molecule limit
-
n∞ ∼ 0.7)
-
(1971)
AIAA Journal
, vol.9
, Issue.7
, pp. 1434-1435
-
-
Phillips1
Kuhlthau2
-
17
-
-
84915463202
-
Subsonic and supersonic static aerodynamic characteristics of a family of bulbous base cones measured with a magnetic suspension and balance system
-
(1972)
NASA CR-1932
-
-
Vlajinac1
-
19
-
-
85058249019
-
Wind tunnel measurements of the roll aerodynamics of the Iroquois sounding rocket and the basic finner using a magnetic model suspension system
-
p )
-
(1967)
MIT TR-137
-
-
Copeland1
-
20
-
-
84915463199
-
Sur une méthode de mesure de la pression de culot
-
2nd edition, La Recherche Aeronautique, no. 79
-
(1960)
0 ⋍ 7,6
, pp. 35
-
-
Dubois1
Rogué2
-
22
-
-
0014568928
-
Experimental studies of a laminar hypersonic cone wake
-
Sphere wakes at M-16
-
(1969)
AIAA Journal
, vol.7
, Issue.9
-
-
Murman1
-
23
-
-
84915463198
-
-
D. K. McLaughlin, J. E. Carter and M. Finston, Experimental investigation of the near wake of a magnetically suspended cone at M = 4.3, AIAA Paper 69-186.
-
-
-
-
24
-
-
0015027963
-
Experimental investigation of the mean flow and stability of the laminar supersonic cone wake
-
(1971)
AIAA Journal
, vol.9
, Issue.3
, pp. 479-484
-
-
McLaughlin1
-
25
-
-
84915463197
-
Some preliminary measurements behind cones magnetically suspended in a Mach number 4.3 stream
-
2nd edition, Fluid Physics of Hypersonic Wakes, Preprint no. 19
-
(1967)
Presented at AGARD
, vol.1
-
-
Browand1
Finston2
McLaughlin3
-
27
-
-
0013069065
-
Dynamic and static stability measurements of the basic finner at supersonic speeds
-
2nd edition, U.S. Naval Ordnance Lab
-
(1960)
NAVORD Report 4516
-
-
Chantz1
Groves2
-
28
-
-
85007690429
-
Hypersonic viscous effects on free flight slender cones
-
(1965)
AIAA Journal
, vol.8
, pp. 1391
-
-
Dayman1
-
31
-
-
0012224641
-
A concept of the vortex lift of sharp-edge delta wings based on a leading-edge-suction analogy
-
(1966)
NASA TN D-3767
-
-
Polhamus1
-
33
-
-
84915463193
-
Low-speed-wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges
-
2nd edition, ARC
-
(1961)
R&M No. 3186, Brit.
-
-
Peckham1
-
35
-
-
0242613794
-
Free-flight measurement of sphere drag at subsonic, transonic, supersonic, and hypersonic speeds for continuum, transition and near-free-molecular flow conditions
-
(1971)
AEDC-TR-70-291
-
-
Bailey1
Hiatt2
-
36
-
-
85007699583
-
Subsonic drag spheres at Reynolds numbers from 200 to 10000
-
(Tech. Notes)
-
(1968)
AIAA Journal
, vol.6
, Issue.5
-
-
Goin1
Lawrence2
-
39
-
-
80054702919
-
Roll damping moment measurement for the basic finner at subsonic and supersonic speeds
-
2nd edition, U.S. Naval Ordnance Lab
-
(1964)
NAVORD Report 6652
-
-
Regan1
-
40
-
-
84915463190
-
Air condensation effects at M = 8.5 measured on the drag and wake of a magnetically suspended 20° cone
-
(1970)
RAE TR 70022
-
-
Crane1
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