High Response Dew Point Measurement System for a Supersonic Wind Tunnel | 東京工業大学附属図書館文献データベース

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High Response Dew Point Measurement System for a Supersonic Wind Tunnel

著者名:: Blumenthal, Philip Z. ( NYMA, Inc. )
掲載資料名:: NASA Technical Reports
発行年:: 1996
巻:: 19960015885
号:: NASA-CR-198453
パート:: NAS 1.26:198453
ペーパー番号:: N96-21663
開始ページ:: 1
終了ページ:: 18
総ページ数:: 18
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:	ZA00001432
論文注記:	NAS3-27186

類似資料:

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5 テクニカルペーパー An overview of aeropropulsion wind tunnel productivity improvements at the NASA Lewis Research Center Arrington, Allen, Becks, Edward, Blumenthal, Philip, DeArmon, John, Klann, Gary, Bencic, Timothy, McCartney, Timothy, … American Institute of Aeronautics and Astronautics	11 テクニカルペーパー A High Performance Aircraft Wind Tunnel Test Using Response Surface Methodologies Landman, D., Simpson, J., Mariani, R., Ortiz, F., Britcher, C. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー An overview of aeropropulsion wind tunnel productivity improvements at the NASA Lewis Research Center Klann, Gary, Bencic, Timothy, McCartney, Timothy, Panek, Joe, Rivera, Osvaldo, Roeder, James, Stark, David, Becks, … National Aeronautics and Space Adminstration	12 テクニカルペーパー DESIGN OF SUPERSONIC WIND TUNNEL Hamilton, C. W. National Aeronautics and Space Administration

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