title: Aerodynamic characteristics of two-plane, unswept tapered wings of aspect
 ratio 3 and 3-percent thickness from tests on a transonic bump
title: NACA Research Memorandums
creator: Emerson, Horace F.
creator: Gale, Bernard M.
contributor: Ames Aeronautical Laboratory (U.S.)
date: 1952-05-02
language: English
description: From Introduction: "The Ames Aeronautical Laboratory has in
 progress an experimental investigation of the aerodynamic characteristics of
 wings of interest in the design of high-speed fighter aircraft. This program
 included an investigation in the Ames 6-by 6-foot supersonic wind tunnel at
 both subsonic and supersonic Mach numbers of a wing-body combination having a
 3-percent-thick, unswept, tapered wing with circular-arc sections and an
 aspect ratio of 3.1 (reference 1).
subject: wind tunnels
subject: wings
rights: Public
rights: Public Domain
rights: No Copyright, Unclassified, Unlimited, Publicly available
type: Report
format: 23 p. : ill.
format: Text
identifier: local-cont-no: 93R16325
identifier: url: http://hdl.handle.net/2060/19930087035
identifier: rep-no: NACA-RM-A52C07
identifier: casi: 19930087035
identifier: https://digital.library.unt.edu/ark:/67531/metadc59178/
identifier: ark: ark:/67531/metadc59178