@article{oai:jaxa.repo.nii.ac.jp:00031710,
 author = {松野, 謙一 and 河村, 龍馬 and MATSUNO, Ken-ichi and KAWAMURA, Ryuma},
 issue = {1_A},
 journal = {東京大学宇宙航空研究所報告},
 month = {Feb},
 note = {非軸対称錐体または,有迎角円錐上の熱伝達を伴う層流境界層に対する解か提示される.本理論は, Mooreの理論をFourier級数表示された錐体の場合へと拡張したものてある.以前に本報告て提示した非粘性錐状直に対する解を,境界層外縁条件として用いることにより,基礎方程式が簡略化される.一様流マッハ数M_∞ = 787,迎角α=2°の10°円錐の場合について計算された熱伝達量は,実験とよく一致した本理論の応用例として,3種の非軸対称錐休の場合について,熱伝達量を計算した。その結果,井粘性流領域における三次元効果か,境界肩中における熱伝達に対して,大きな影響を及すことか示された., A solution to the laminar boundary layer equation with heat-transfer on the conical body, of which the cross-section is assumed to be nearly circular but otherwise arbitrary, is presented Present theory is the extension of Moore's to the cases of non-axisymmetric conical bodies given by Fourier series. A solution for the outer nonviscous flow, presented previously in this report, is available and simplifies the basic equation. The predicted heat-transfer to the 10° semi-apex circular cone at 2° angle of attack at M_∞,=7.87 agrees with the experimental value fairly well. As an example, present theory is applied to the cases of several shapes of nonaxisymmetric conical bodies at M_∞=50. The results show that a small three-dimensional effect in the outer nonviscous flow causes a large effect on the heat-transfer in the boundary layer., 資料番号: SA0124731000},
 pages = {53--65},
 title = {錐体上の熱伝達を伴う層流境界層},
 volume = {13},
 year = {1977}
}