Your cart is empty

NASA-CR-3449-1981 Calculation of vortex lift effect for cambered

$43.80

The files are in electronic format PDF (Networkable/Copy/Paste) (English) and will be sent to your email in hours.
Standard Title: Calculation of vortex lift effect for cambered wings by the suction analogy
Standard NO.:NASA-CR-3449-1981
Papges: 86


Add to Cart:

  • 1000 Units in Stock


This product was added to our catalog on Saturday 09 July, 2016.

walitefree