Surface and Flow Field Measurements in a Symmetric Crossing Shock Wave/Turbulent Boundary-Layer Interaction

Surface and Flow Field Measurements in a Symmetric Crossing Shock Wave/Turbulent Boundary-Layer Interaction

著者名:

Davis, D.O. ( National Aeronautics and Space Administration Lewis Reseaech Center )
Hingst, W.R.

掲載資料名:

NASA Technical Reports

発行年:

1992

号:

NASA-TM-106086

パート:

NAS 1.15:106086

ペーパー番号:

N93-24911

開始ページ:

1

終了ページ:

20

総ページ数:

20

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00001429

類似資料:

1 テクニカルペーパー Experimental investigation of crossing shock wave - turbulent boundary layer - bleed interaction Kim, H.D., Hingst, W.R., Davis, D.O. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー 3-D crossing shock wave - turbulent boundary layer interaction Gnedin, M., Knight, D., Zheltovodov, A., Maksimov, A., Shevchenko, A., Vorontsov, S. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Experimental Investigation of Crossing Shock Wave-Turbulent Boundary Layer-Bleed Interaction Kim, Hyun, Hingst, Warren R., Davis, David O. National Aeronautics and Space Adminstration	8 テクニカルペーパー Flowfield Measurements Inside a Boundary-Layer Bleed Slot Davis, D. O., Willis, B. P., Hingst, W. R. National Aeronautics and Space Adminstration
3 テクニカルペーパー Interaction of Two Glancing, Crossing Shock Waves With a Turbulent Boundary-Layer at Various Mach Numbers Hingst, Warren R., Williams, Kevin E. National Aeronautics and Space Adminstration	9 テクニカルペーパー Computational of crossing glancing shocks - turbulent boundary layer interaction with bleed Reddy, D.R. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Flow Coefficient Behavior for Boundary Layer Bleed Holes and Slots Willis, B.P., Davis, D.O., Hingst, W.R. National Aeronautics and Space Adminstration	10 テクニカルペーパー SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION IN THE FLOW FIELD OF A TRI-DIMENSION WIND TUNNEL Benay, R. National Aeronautics and Space Administration
5 テクニカルペーパー Experimental investigation of the effect of a single bleed hole on a supersonic turbulent boundary-layer Bodner, J.P., Greber, I., Davis, D.O., Hingst, W.R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Compressible turbulence measurements in a supersonic boundary layer with impinging shock wave interaction Meyer, M.J., Buter, T.A., Bowersox, R.D.W. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Evaluation of a Technique To Generate Artificially Thickened Boundary Layers in Supersonic and Hypersonic Flows Porro, A.R., Hingst, W.R., Davis, D.O., Blaie, A.B., Jr. National Aeronautics and Space Adminstration	12 テクニカルペーパー Numerical Investigation of New Topologies in Strong Crossing Shock-Wave/Turbulent Boundary Layer Interactions Schmisseur, J. D., Gaitonde, Datta V. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12