diff options
| -rw-r--r-- | science/Makefile | 1 | ||||
| -rw-r--r-- | science/aircraft-datcom/Makefile | 24 | ||||
| -rw-r--r-- | science/aircraft-datcom/distinfo | 3 | ||||
| -rw-r--r-- | science/aircraft-datcom/pkg-descr | 15 | ||||
| -rw-r--r-- | science/aircraft-datcom/pkg-plist | 4 |
5 files changed, 47 insertions, 0 deletions
diff --git a/science/Makefile b/science/Makefile index 0236a4b7db27..5748d3013f9f 100644 --- a/science/Makefile +++ b/science/Makefile @@ -20,6 +20,7 @@ SUBDIR += R-cran-som SUBDIR += R-cran-udunits2 SUBDIR += afni + SUBDIR += aircraft-datcom SUBDIR += avogadro SUBDIR += bddsolve SUBDIR += bft diff --git a/science/aircraft-datcom/Makefile b/science/aircraft-datcom/Makefile new file mode 100644 index 000000000000..54ceebb0c6c3 --- /dev/null +++ b/science/aircraft-datcom/Makefile @@ -0,0 +1,24 @@ +# $FreeBSD$ + +PORTNAME= aircraft-datcom +DISTVERSION= 0.0.20120723 +CATEGORIES= science + +MAINTAINER= mike.d.ft402@gmail.com +COMMENT= Modified USAF Aircraft Stability and Control Data Compendium + +LICENSE= GPLv3 + +USE_GITHUB= yes +GH_ACCOUNT= arktools +GH_TAGNAME= ed877bb + +USES= fortran cmake + +.include <bsd.port.pre.mk> + +post-install: + ${MKDIR} ${STAGEDIR}${DOCSDIR} + ${INSTALL_MAN} ${WRKSRC}/doc/* ${STAGEDIR}${DOCSDIR} + +.include <bsd.port.post.mk> diff --git a/science/aircraft-datcom/distinfo b/science/aircraft-datcom/distinfo new file mode 100644 index 000000000000..cb4aff8ce93d --- /dev/null +++ b/science/aircraft-datcom/distinfo @@ -0,0 +1,3 @@ +TIMESTAMP = 1484250474 +SHA256 (arktools-aircraft-datcom-0.0.20120723-ed877bb_GH0.tar.gz) = e9c8e5cf55f179bf3e3fa0aa27d238455822cc491afebe11b7548661c666f598 +SIZE (arktools-aircraft-datcom-0.0.20120723-ed877bb_GH0.tar.gz) = 38664179 diff --git a/science/aircraft-datcom/pkg-descr b/science/aircraft-datcom/pkg-descr new file mode 100644 index 000000000000..07bf553be5cc --- /dev/null +++ b/science/aircraft-datcom/pkg-descr @@ -0,0 +1,15 @@ +This computer program calculates static stability, high lift and control, and +dynamic derivative characteristics using the methods contained in the USAF +Stability and Control Datcom (Data Compendium). Configuration geometry, +attitude, and Mach range capabilities are consistent with those accommodated by +the Datcom. The program contains a trim option that computes control +deflections and aerodynamic increments for vehicle trim at subsonic Mach +numbers. + +WWW: http://www.pdas.com/datcom.html + +This project is a modified version of the publically released USAF aircraft +datcom. The goal of the project is to update the code and make it more usable +by the end user. + +WWW: https://github.com/arktools/aircraft-datcom diff --git a/science/aircraft-datcom/pkg-plist b/science/aircraft-datcom/pkg-plist new file mode 100644 index 000000000000..185ee8200a13 --- /dev/null +++ b/science/aircraft-datcom/pkg-plist @@ -0,0 +1,4 @@ +bin/aircraft-datcom +bin/aircraft-datcom-plot +%%PORTDOCS%%%%DOCSDIR%%/Users'_Manual Vol_1.pdf +%%PORTDOCS%%%%DOCSDIR%%/Users'_Manual Vol_2.pdf |