CORE
🇺🇦
make metadata, not war
Services
Services overview
Explore all CORE services
Access to raw data
API
Dataset
FastSync
Content discovery
Recommender
Discovery
OAI identifiers
OAI Resolver
Managing content
Dashboard
Bespoke contracts
Consultancy services
Support us
Support us
Membership
Sponsorship
Community governance
Advisory Board
Board of supporters
Research network
About
About us
Our mission
Team
Blog
FAQs
Contact us
research
Nose controls on delta wings at supersonic speeds
Authors
B. W. Bolton Shaw
Publication date
1 May 1950
Publisher
College of Aeronautics, Cranfield.
Abstract
Expressions are derived for lξ and a2 of nose ailerons and nose elevators on a delta wing, as depicted in Fig. 1, in supersonic flight. Nose and trailing edge controls on delta wings in supersonic flight are compared
Similar works
Full text
Open in the Core reader
Download PDF
Available Versions
Cranfield CERES
See this paper in CORE
Go to the repository landing page
Download from data provider
oai:dspace.lib.cranfield.ac.uk...
Last time updated on 01/07/2012