Skip to Main Content
Article navigation
Volume 33, Issue 1
1 January 1961
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 33, Issue 1
Review Article| January 01 1961

Calculation of Supersonic Aerodynamic Influence Matrices: A Numerical Method for Wings of Arbitrary Planform Suitable for Solution on the Digital Computer

T.H. Hallstaff, B.Sc., A.C.G.I.
T.H. Hallstaff, B.Sc., A.C.G.I.
Search for other works by this author on:
This Site
PubMed
Google Scholar
Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1961
Aircraft Engineering (1961) 33 (1): 16–19.
https://doi.org/10.1108/eb033356

This paper describes a routine for calculating supersonic aerodynamic influence matrices, which is suitable for the digital computer. The method is first applied to a wing with straight leading edges, streamwise tips and a supersonic trailing edge. Then, an extension is given which enables wings of arbitrary planform (including those with subsonic trailing edges) to be treated without revision of the original programme.

This content is only available via PDF.
© MCB UP Limited
1961
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.

Please enter valid email address.
Email address must be 94 characters or fewer.
Pay-Per-View Access
$39.00
Rental
This article is also available for rental through DeepDyve. Read this now at DeepDyve
106 Views
View Metrics
Development and validation of a perceived aviation risk scale: evidence from public samples
Dynamic energy harvesting in unpowered flight: empirical flight mechanics and aerodynamic design implications
Integrated design method of aircraft RBF neural network-based fault diagnosis and nonlinear dynamic inversion control
A comparative analysis of YOLO lightweight models for foreign object detection at airports

Suggested Reading

Geometrical and roughness effects on compound channel resistance
Proceedings of the Institution of Civil Engineers - Water and Maritime Engineering (September,2000)
Static equilibrium bays in coast protection
Maritime Engineering (June,2007)
Helicopter stabilizer optimization considering rotor downwash in forward-flight
Aircraft Engineering and Aerospace Technology: An International Journal (October,2016)
British Research Aircraft: Brief Details of Two Single‐seat Research Aircraft Produced by the British Aircraft Corporation
Aircraft Engineering (October,1962)
Design and testing of fixed‐wing MAVs
Aircraft Engineering and Aerospace Technology: An International Journal (July,2007)

Related Chapters

Planform models for bayed beaches: the influence of breakwaters and stream discharges
Breakwaters, coastal structures and coastlines: Proceedings of the international conference organized by the Institution of Civil Engineers and held in London, UK on 26-28 September 2001
CAMBRILS BEACH EROSION PROBLEM: A CASE STUDY
Solving Coastal Conundrums
The Hythe to Folkestone harbour coast protection scheme - The use of rock headlands to create static equilibrium bays
International Conference on Coastlines, structures and breakwaters 2005

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