SNI 2372 5-2011 Cara uji fisika - Bagian 5 Penentuan rasio penyerapan air (RPA) pada produk perikanan.pdf

上传人:刘芸 文档编号:1051151 上传时间:2019-03-27 格式:PDF 页数:12 大小:225.36KB
下载 相关 举报
SNI 2372 5-2011 Cara uji fisika - Bagian 5 Penentuan rasio penyerapan air (RPA) pada produk perikanan.pdf_第1页
第1页 / 共12页
SNI 2372 5-2011 Cara uji fisika - Bagian 5 Penentuan rasio penyerapan air (RPA) pada produk perikanan.pdf_第2页
第2页 / 共12页
SNI 2372 5-2011 Cara uji fisika - Bagian 5 Penentuan rasio penyerapan air (RPA) pada produk perikanan.pdf_第3页
第3页 / 共12页
SNI 2372 5-2011 Cara uji fisika - Bagian 5 Penentuan rasio penyerapan air (RPA) pada produk perikanan.pdf_第4页
第4页 / 共12页
SNI 2372 5-2011 Cara uji fisika - Bagian 5 Penentuan rasio penyerapan air (RPA) pada produk perikanan.pdf_第5页
第5页 / 共12页
点击查看更多>>
资源描述
展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-ARR-L5F06-1945 Wind-tunnel investigation of control-surface characteristics XXII - medium and large aerodynamic balances of two nose shapes and a plain overhang used withrfoi.pdf NASA NACA-ARR-L5F06-1945 Wind-tunnel investigation of control-surface characteristics XXII - medium and large aerodynamic balances of two nose shapes and a plain overhang used withrfoi.pdf
  • NASA NACA-ARR-L5G25-1945 Wind tunnel investigation of control-surface characteristics XXIII  a 0 25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 .pdf NASA NACA-ARR-L5G25-1945 Wind tunnel investigation of control-surface characteristics XXIII a 0 25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 .pdf
  • NASA NACA-ARR-L6A05-1946 Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates《平面矩形板纵向和横向直接应力临界组合图》.pdf NASA NACA-ARR-L6A05-1946 Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates《平面矩形板纵向和横向直接应力临界组合图》.pdf
  • NASA NACA-CB-5B05-1945 Computation of hinge-moment characteristics of horizontal tails from section data《根据截面数据对水平尾翼铰链力矩特性的计算》.pdf NASA NACA-CB-5B05-1945 Computation of hinge-moment characteristics of horizontal tails from section data《根据截面数据对水平尾翼铰链力矩特性的计算》.pdf
  • NASA NACA-CB-L4G10-1944 Wind tunnel investigation of NACA 66(215)-216 66 1-212 and 65(sub 1)-212 airfoils with 0 20-airfoil-chord split flaps《对带有0 20翼弦分裂式襟翼NACA 66(215)-216 66 1-21.pdf NASA NACA-CB-L4G10-1944 Wind tunnel investigation of NACA 66(215)-216 66 1-212 and 65(sub 1)-212 airfoils with 0 20-airfoil-chord split flaps《对带有0 20翼弦分裂式襟翼NACA 66(215)-216 66 1-21.pdf
  • NASA NACA-CB-L5C01-1945 Estimation of stick-fixed neutral points of airplanes《飞机固定驾驶杆中性点估计》.pdf NASA NACA-CB-L5C01-1945 Estimation of stick-fixed neutral points of airplanes《飞机固定驾驶杆中性点估计》.pdf
  • NASA NACA-CR-195480-1996 Improved NASA-ANOPP Noise Prediction Computer Code for Advanced Subsonic Propulsion Systems Volume 1 ANOPP Evaluation and Fan Noise Model Improvement《先进亚音速.pdf NASA NACA-CR-195480-1996 Improved NASA-ANOPP Noise Prediction Computer Code for Advanced Subsonic Propulsion Systems Volume 1 ANOPP Evaluation and Fan Noise Model Improvement《先进亚音速.pdf
  • NASA NACA-CR-3675-1983 An aerodynamic analysis computer program and design notes for low speed wing flap systems《空气动力分析计算机程序和低速襟翼系统的设计说明》.pdf NASA NACA-CR-3675-1983 An aerodynamic analysis computer program and design notes for low speed wing flap systems《空气动力分析计算机程序和低速襟翼系统的设计说明》.pdf
  • NASA NACA-CR-793-1967 STOP - A computer program for supersonic transport trajectory optimization《停止 超音速运输机轨道优化的计算机程序》.pdf NASA NACA-CR-793-1967 STOP - A computer program for supersonic transport trajectory optimization《停止 超音速运输机轨道优化的计算机程序》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1