Engineering Virtual Library
Creating & Delivering The World's Finest Aviation Experience

EVL Archive

34061 - 34070 of 34281 results found

STRUCTURAL ANALYSIS POSTPROCESSING UTILITIES

Subjects
Structural Analysis
Record Type
TECHRPT
Corporate Author
University of Dayton Research Institute, Dayton, OH
Author
Brockman, R A|Wright, M E|Bouchard, M P
Project Number
F33615-80-C-3403
Iron Mountain Box Number
IM - 723191191
Publication Date
2022

STRUCTURAL DESIGN DATA

Record Type
Book
Corporate Author
Grumman Aircraft Engineering, Bethpage, NY
Iron Mountain Box Number
IM - 649034295
Publication Date
2022

STRUCTURAL DESIGN LOADS (SECTION 0 - GENERAL)

Corporate Author
Grumman Aircraft Engineering, Bethpage, NY
Pages
66
Author
Renkewitz, F
Notes
One section of a 12 part report
Description
A - Extended Range Tip Tanks (28 January 1977)|B - Aviation Partners Winglet - General (19 March 1993)|C - ASC 451 Quiet Spey Modifications (18 June 1993)
Publication Date
2065

STRUCTURAL DESIGN LOADS (SECTION IV - WING)

Corporate Author
Grumman Aircraft Engineering, Bethpage, NY
Pages
618
Author
Luhrssen, R
Notes
One section of a 12 part report
Description
A - Effect of Increased RGW to 56,500 LB (2 October 1967)|B - Wing Gust Loads (3 February 1977)|C - Effect of Increased RGW to 58,000 LB (14 October 1967)|D - Effect of Increased RGW to 60,000 LB (4 October 1968)|E - Effect of Increased RGW to 62,500 LB (24 November 1969)|F - Design Loads not Covered In Appendix M, Section II for 65,300 LB RGW (4 February 1977)
Publication Date
2065

STRUCTURAL DESIGN LOADS (SECTION V - HORIZONTAL TAIL LOADS)

Corporate Author
Grumman Aircraft Engineering, Bethpage, NY
Pages
140
Author
Pittel, M
Notes
One section of a 12 part report
Description
A - Effect of Increased RGW to 56,500 LB (2 October 1967)|B - Effect of Increased RGW to 58,000 LB (14 October 1967)|C - Effect of Increased RGW to 60,000 LB (1 Auguat 1968)|D - Effect of Increased RGW to 62,500 LB (8 December 1969)
Publication Date
2065

STRUCTURAL DESIGN LOADS (SECTION VII - FUSELAGE LOADS)

Corporate Author
Grumman Aircraft Engineering, Bethpage, NY
Pages
124
Author
Brodman, H
Notes
One section of a 12 part report
Description
A - Effect of Increased RGW to 56,500 LB (27 October 1967)|B - Additional Fuselage Loads (13 October 1967)|C - Effect of Increased RGW to 58,000 LB (14 October 1967)|D - Additional Fuselage Loads (26 February 1968)|E - Effect of Increased RGW to 60,000 LB (4 October 1968)|F - Effect of Increased RGW to 62,500 LB (20 May 1970)
Publication Date
2065

STRUCTURAL DESIGN LOADS (SECTION VIII - AEROELASTICITY)

Corporate Author
Grumman Aircraft Engineering, Bethpage, NY
Pages
56
Author
Mohrman, R
Notes
One section of a 12 part report
Description
A - Additional Aeroelasticity (15 June 1967)|B - Effect of Tip Tanks on Aeroelasticity (7 April 1976)|C - Aviation Partners Winglet - Aeroelasticity (19 March 1993)
Publication Date
2065