column
Numerical analysis for correlation of standard model testing in high enthalpy facility and flight test
, ,
2002, 16(2): 1-8,20. DOI: 10.3969/j.issn.1672-9897.2002.02.001
Abstract PDF
Three-dimensional parallel simulation of the flow-field of a scramjet combustor and comparisons with experiments
,
2002, 16(2): 9-15. DOI: 10.3969/j.issn.1672-9897.2002.02.002
Abstract PDF
On the correlation of force test results of a tactical missile calibration model in five different wind tunnels
, , , , , ,
2002, 16(2): 16-20. DOI: 10.3969/j.issn.1672-9897.2002.02.003
Abstract PDF
Study on flow patterns over spur-dikes
, ,
2002, 16(2): 21-24,83. DOI: 10.3969/j.issn.1672-9897.2002.02.004
Abstract PDF
An investigation of increasing lift on large transport by using Gurney flap positioned at the trailing-edge
, , ,
2002, 16(2): 25-29. DOI: 10.3969/j.issn.1672-9897.2002.02.005
Abstract PDF
Effect of Gurney flaps on aerodynamical characters of single airfoil
, ,
2002, 16(2): 30-35. DOI: 10.3969/j.issn.1672-9897.2002.02.006
Abstract PDF
A direct experimental simulation of side-jet steering
, , ,
2002, 16(2): 36-41. DOI: 10.3969/j.issn.1672-9897.2002.02.007
Abstract PDF
Experimental investigation on cavitation noise of an axisymmetric body
, , ,
2002, 16(2): 42-46. DOI: 10.3969/j.issn.1672-9897.2002.02.008
Abstract PDF
Numerical Simulation of flame deformation induced by obstacle
, ,
2002, 16(2): 47-51. DOI: 10.3969/j.issn.1672-9897.2002.02.009
Abstract PDF
Effect of the apex flap on the leading edge vortex breakdown over a 70° delta wing
, ,
2002, 16(2): 52-56. DOI: 10.3969/j.issn.1672-9897.2002.02.010
Abstract PDF
The design techniques of hypersonic Teflon cone and sabot for hypervelocity ballistic range tests
,
2002, 16(2): 57-62. DOI: 10.3969/j.issn.1672-9897.2002.02.011
Abstract PDF
Boundary layer simulation in the first test section of 8m×6m wind tunnel
, ,
2002, 16(2): 63-66. DOI: 10.3969/j.issn.1672-9897.2002.02.012
Abstract PDF
The location of boundary-layer transition detected by pressure fluctuation measurements
, , ,
2002, 16(2): 67-71. DOI: 10.3969/j.issn.1672-9897.2002.02.013
Abstract PDF
The measurement on the turbulence jet with 3D LDV system
,
2002, 16(2): 72-77. DOI: 10.3969/j.issn.1672-9897.2002.02.014
Abstract PDF
Particle recognition of PTV measurement in gas-particle two-phase flow using fuzzy logic method
, , , ,
2002, 16(2): 78-83. DOI: 10.3969/j.issn.1672-9897.2002.02.015
Abstract PDF
Development and application of advance air source system for wind tunnel
2002, 16(2): 84-87. DOI: 10.3969/j.issn.1672-9897.2002.02.016
Abstract PDF
The survey of the inertia moment in free flight models
2002, 16(2): 88-91. DOI: 10.3969/j.issn.1672-9897.2002.02.017
Abstract PDF
Test technique and application of large-scale pressure measurement in the 2.4m×2.4m transonic wind tunnel
, ,
2002, 16(2): 92-96. DOI: 10.3969/j.issn.1672-9897.2002.02.018
Abstract PDF

Submit Article

Submission Guidelines

Contact Us

Qrcode