{"id":557393,"date":"2024-11-05T18:17:53","date_gmt":"2024-11-05T18:17:53","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/esdu-070022011\/"},"modified":"2024-11-05T18:17:53","modified_gmt":"2024-11-05T18:17:53","slug":"esdu-070022011","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/esdu\/esdu-070022011\/","title":{"rendered":"ESDU 07002:2011"},"content":{"rendered":"
Viscous drag coefficient is defined in ESDU 07002 as the drag
\ncoefficient arising from all the effects of viscosity. Equations
\nand graphs are provided for predicting the viscous drag coefficient
\nof wings with sweep angles not exceeding 45\u00b0, aspect ratios not
\nexceeding 12, maximum section thickness to chord ratios within the
\nrange 0.1 to 0.2 and up to 10\u00b0 wash-in or wash-out.<\/p>\n
ESDU 07002 is applicable to values of lift coefficient at which
\nboth upper and lower surface boundary layers are fully attached, in
\nflow fields where shockwaves are not present. The method is
\napplicable to both straight-tapered and cranked wing planforms and
\nwhere the section geometry, including camber, either remains
\nunaltered or varies with spanwise location. Knowledge of a constant
\nchordwise location of boundary-layer transition across the span is
\nrequired. The method is based on a semi-empirical investigation
\nusing strip theory presented in ESDU 07003.<\/p>\n
As a means of testing the validity of the method, polars of Wing viscous drag coefficient in shock-free attached flow<\/b><\/p>\n
\npredicted and measured total drag coefficient for five wing
\ngeometries are compared. The predicted total drag coefficient was
\nobtained by adding values of inviscid trailing-vortex drag
\ncoefficient (predicted using ESDU 10022) to values of viscous drag
\ncoefficient obtained by the method of this Data Item. In most cases
\nthere is agreement to within about 10 drag counts
\n(CD<\/sub><\/i> = 0.001) between the predicted data and the
\ntest data, over the ranges of lift coefficient where the boundary
\nlayers are indicated as being fully attached. The method is
\nappropriate for initial project calculations, where an agreement to
\nwithin 10 drag counts might be considered reasonable if the effects
\nof configuration changes rather than absolute values are of
\ninterest.<\/p>\n","protected":false},"excerpt":{"rendered":"\n\n
\n Published By<\/td>\n Publication Date<\/td>\n Number of Pages<\/td>\n<\/tr>\n \n ESDU<\/b><\/a><\/td>\n 2011-12-01<\/td>\n 62<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n","protected":false},"featured_media":557402,"template":"","meta":{"rank_math_lock_modified_date":false,"ep_exclude_from_search":false},"product_cat":[2675],"product_tag":[],"class_list":{"0":"post-557393","1":"product","2":"type-product","3":"status-publish","4":"has-post-thumbnail","6":"product_cat-esdu","8":"first","9":"instock","10":"sold-individually","11":"shipping-taxable","12":"purchasable","13":"product-type-simple"},"_links":{"self":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product\/557393","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product"}],"about":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/types\/product"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media\/557402"}],"wp:attachment":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media?parent=557393"}],"wp:term":[{"taxonomy":"product_cat","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_cat?post=557393"},{"taxonomy":"product_tag","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_tag?post=557393"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}