Update search
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
NARROW
Format
Journal
Type
Date
Availability
1-4 of 4
P. Person
Close
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Journal Articles
Semi‐Articulated Bogie Undercarriage Landing Performance: Analysis of a Type Used on Large Aircraft
Available to Purchase
Aircraft Engineering (1959) 31 (1): 2–5.
Published: 01 January 1959
Journal Articles
Stability and Strength of an Undercarriage Radius Rod: A Study of the Structural Design Criteria of an Articulated Radius Rod with an Internally Locked Jack
Available to Purchase
Aircraft Engineering (1954) 26 (5): 154–156.
Published: 01 May 1954
Journal Articles
The Semi‐articulated Multi‐wheel Bogie Undercarriage: A Statement of the Problems Involved Together with a Description of one Method of Overcoming Them
Available to Purchase
Aircraft Engineering (1951) 23 (4): 104–106.
Published: 01 April 1951
Journal Articles
The Strength of Jacks in Compression: Methods Suitable for Determining the Compressive Strength of Jacks Which May Be Locked Internally or Externally
Available to Purchase
Aircraft Engineering (1949) 21 (4): 113–115.
Published: 01 April 1949
