Article navigation
Volume 30, Issue 7
1 July 1958
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 30, Issue 7
Review Article| July 01 1958

Tools for the Workshop

Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1958
Aircraft Engineering (1958) 30 (7): 218.
https://doi.org/10.1108/eb032996

The instrument shown in FIG. 1 has been designed for the accurate projection of the leading edges of scale prototype aerofoils in Research Establishments. It provides an accurate form of the leading edge section magnified twenty times in the direction of airflow on wings having a sweepback from 15–55 deg.

This content is only available via PDF.
© MCB UP Limited
1958
You do not currently have access to this content.
Don't already have an account? Register

Purchased this content as a guest? Enter your email address to restore access.

Pay-Per-View Access
$39.00
Rental
This article is also available for rental through DeepDyve. Read this now at DeepDyve
86 Views

New and popular articles

A fail-safe decision-support framework for onboard greywater reuse in commercial aircraft water systems
Dual-state estimation of electric vertical take-off and landing batteries: data-driven modeling and experimental verification
Development of 7XXX-Al series composite materials using high-speed mechanical alloying
Inverse finite element framework for aeroelastic integration of black-box subsystems under intellectual property constraints

Suggested Reading

Aircraft with Variable‐Sweep Wings: A Discussion Outlining the Advantages and Disadvantages of Variable‐Sweep Aircraft and the Principal Features of Three Possible Types: a Trainer, a Strike Fighter and a Supersonic Transport
Aircraft Engineering (October,1965)
Some Structural Parameters for an Aero‐Isoclinic Wing: A Novel Method of Building an Aero‐Isoclinic Wing
Aircraft Engineering (September,1952)
EMB‐145 has Revised Configuration
Aircraft Engineering (April,1991)
Rotary Derivatives in Yaw: Calculation by Lifting Plane Theory of the Rolling and Yawing Moments of a Wing Due to Rotary Motion in Yaw
Aircraft Engineering (February,1951)
Sweepback and Wing Taper: The Effect of Sweepback on the Lift, Drag, and Aerodynamic Centre of a Tapered Wing
Aircraft Engineering (October,1950)

Related Chapters

8. The Briefing Workshop
Value Management: The value management benchmark: A good practice framework for clients and practitioners
7. The Pre-Brief Workshop
Value Management: The value management benchmark: A good practice framework for clients and practitioners
5. The Value Management Workshop Process
Value Management: The value management benchmark: A good practice framework for clients and practitioners

Recommended for you

These recommendations are informed by your reading behaviors and indicated interests.

Cited By

Google Scholar
This Feature Is Available To Subscribers Only

or Create an Account

Close Modal
Close Modal