🔥🔥 Don’t Miss Out on Our End of Autumn Sale. If you have any questions, feel free to click the bottom right corner to contact our customer service..

Concat us[email protected]
Shopping Cart

No products in the cart.

ESDU AERO W.01.01.01:1989

ESDU AERO W.01.01.01:1989

$62.40

Lift-curve slope of swept and tapered wings

Published By Publication Date Number of Pages
ESDU 1989-10-01 5
PDF Format Searchable Printable Preview Now
Guaranteed Safe Checkout
Category:

If you have any questions, feel free to reach out to our online customer service team by clicking on the bottom right corner. We’re here to assist you 24/7.
Email:[email protected]

ESDU Aero W.01.01.01 has been superseded by ESDU 70011, which presents graphs of correlated lifting-surface theory results, but is retained in the Series because values from it must be used when obtaining lift-dependent drag of plane, symmetric-section wings using ESDU 66032 and in evaluating the wing dihedral contribution to the rolling moment in sideslip using ESDU Aero A.06.01.03 and ESDU Aero A.06.01.09. Otherwise ESDU 70011 should always be used to evaluate the lift-curve slope for swept and tapered wings at subsonic speeds.

Related products

ESDU AERO W.01.01.01:1989
$62.40