Accession Number:

AD0248516

Title:

Wind Tunnel Tests and Further Analysis of the Floating Wing Fuel Tanks for Helicopter Range Extension (Helicopter Range Extension Wind Tunnel Study, Vol. 1)

Descriptive Note:

Corporate Author:

BOEING CO MORTON PA VERTOL DIV

Personal Author(s):

Report Date:

1960-10-17

Pagination or Media Count:

152.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE