Wind-tunnel tests of several arrangements of external auxiliary fuel tanks on a fighter-type airplane / by Edward Pepper.

An investigation was conducted in the NACA 19-foot pressure tunnel to detemine the aerodynamic effices of several arrangements of external auxiliary fuselage and wing tanks of large fuel capacity on a fighter-type airplane. Model tank arrangements tested were 350-gallon rectangular cross section tan...

Full description

Saved in:
Bibliographic Details
Main Author: Pepper, Edward
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L371.
Subjects:

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L371
Y 3.N 21/5:11/L371 Available Place a Hold