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Laminar flow control for aircraft lessons from the past and prospects for the future AIAA-2000-2540

Laminar flow control for aircraft lessons from the past and prospects for the future AIAA-2000-2540
Paper規格・テクニカルリポート類
Poll, D. I. A2000<M-AIAA-2000-2540>
National Diet Library

Instability and transition of flow at, and near, an attachment-line [microform] : including control by surface suction / A. Smith and D.I.A. Poll ([NASA contractor report] ; NASA/CR-1998-208443)

Instability and transition of flow at, and near, an attachment-line [microform] : including control by surface suction / A. Smith and D.I.A. Poll ([NASA contractor report] ; NASA/CR-1998-208443)
Microform図書
1998<YCA-NAS 1.26:208443>
National Diet Library
  • Author HeadingSmith, A Poll, D. I. A Langley Research Center

Experimental and computational investigation of leading edge transition at Mach 1.6 AIAA-97-1776

Experimental and computational investigation of leading edge transition at Mach 1.6 AIAA-97-1776
Paper規格・テクニカルリポート類
Coleman, Colin P, Poll, D. I. A, Lin, Ray-Sing1997<M-AIAA-97-1776>
National Diet Library

The effect of wing sweep back upon transition in hypersonic flow AIAA-95-6090

The effect of wing sweep back upon transition in hypersonic flow AIAA-95-6090
Paper規格・テクニカルリポート類
Poll, D. I. A1995<M-AIAA-95-6090>
National Diet Library

Natural and hybrid laminar flow control for aero-engine nacelles SAE-952016

Natural and hybrid laminar flow control for aero-engine nacelles SAE-952016
Paper規格・テクニカルリポート類
Mullender, A. J, Poll, D. I. A1995<M-SAE-952016>
National Diet Library

Instability and transition of flow at, and near, an attachment-line [microform] : including control by surface suction : contract number NCC1-218 / A. Smith and D.I.A. Poll

Instability and transition of flow at, and near, an attachment-line [microform] : including control by surface suction : contract number NCC1-218 / A. Smith and D.I.A. Poll
Microform図書
1996<YCA-NAS 1.26:207496>
National Diet Library
  • Author HeadingSmith, A Poll, D. I. A United States. National Aeron...

NOTE ON THE ALGEBRAIC REPRESENTATION OF THE PRESTON TUBE CALIBRATION. (CAR ; CAR-8308)

NOTE ON THE ALGEBRAIC REPRESENTATION OF THE PRESTON TUBE CALIBRATION. (CAR ; CAR-8308)
Paper図書
POLL, D.I.A.1983.
Other Libraries in Japan

NOTE ON THE USE OF SURFACE PITOT TUBES FOR THE MEASUREMENT OF SKIN FRICTION IN LAMINAR BOUNDARY LAYERS. (REPT ; REPT-8307)

NOTE ON THE USE OF SURFACE PITOT TUBES FOR THE MEASUREMENT OF SKIN FRICTION IN LAMINAR BOUNDARY LAYERS. (REPT ; REPT-8307)
Paper図書
POLL, D.I.A.1983.
Other Libraries in Japan

Stability of an Infinite Swept Attachment Line Boundary Layer. Final Report NASA-CR-172300 N84-19285 NAS-126172300 ICASE-845

Stability of an Infinite Swept Attachment Line Boundary Layer. Final Report NASA-CR-172300 N84-19285 NAS-126172300 ICASE-845
Microform規格・テクニカルリポート類
Hall, P, Mallik, M. R, Poll, D. I. A<LS-N84/19285>
National Diet Library

Reynolds number effects on the flow around 2-D ellipses at incidence AIAA-95-0366

Reynolds number effects on the flow around 2-D ellipses at incidence AIAA-95-0366
Paper規格・テクニカルリポート類
Lamont, P. J, Poll, D. I. A, Taghavi-Zenouz, R<M-AIAA-95-0366>
National Diet Library

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