Hypersonic Aircraft Design Project

AI Thread Summary
The discussion highlights a report valuable for Aerospace Engineering professionals, focusing on the design aspects of hypersonic aircraft. The report provides detailed insights that can aid in understanding the complexities involved in hypersonic flight. Participants express appreciation for the shared resource, emphasizing its relevance to current aerospace projects. The link to the report is included for easy access to the information. This resource is positioned as a significant contribution to the field of hypersonic aircraft design.
Engineering news on Phys.org
You truley know how to snoop out hte most interesting things and link to them. You are the Physicsforums search engine :biggrin:
 

Thread 'Race car suspension Class'

Posted June 2024 - 15 years after starting this class. I have learned a whole lot. To get to the short course on making your stock car, late model, hobby stock E-mod handle, look at the index below. Read all posts on Roll Center, Jacking effect and Why does car drive straight to the wall when I gas it? Also read You really have two race cars. This will cover 90% of problems you have. Simply put, the car pushes going in and is loose coming out. You do not have enuff downforce on the right...
View full post »
Thread 'Physics of Stretch: What pressure does a band apply on a cylinder?'

Thread 'Physics of Stretch: What pressure does a band apply on a cylinder?'

Scenario 1 (figure 1) A continuous loop of elastic material is stretched around two metal bars. The top bar is attached to a load cell that reads force. The lower bar can be moved downwards to stretch the elastic material. The lower bar is moved downwards until the two bars are 1190mm apart, stretching the elastic material. The bars are 5mm thick, so the total internal loop length is 1200mm (1190mm + 5mm + 5mm). At this level of stretch, the load cell reads 45N tensile force. Key numbers...
View full post »

Thread 'Cantilever help'

I'm trying to decide what size and type of galvanized steel I need for 2 cantilever extensions. The cantilever is 5 ft. The space between the two cantilever arms is a 17 ft Gap the center 7 ft of the 17 ft Gap we'll need to Bear approximately 17,000 lb spread evenly from the front of the cantilever to the back of the cantilever over 5 ft. I will put support beams across these cantilever arms to support the load evenly
View full post »

Similar threads

Mechanical/Aerospace Engineering Undergrad Senior Design Project
Replies
3
Views
2K
Need help on designing a conceptual HALE UAV
Replies
11
Views
2K
Can someone explain this engine to me?
Replies
1
Views
2K
Can Damping Values for Aluminum Cantilever Beams Be Easily Found?
Replies
2
Views
2K
Working for defense company?
Replies
16
Views
303
Thermal effects in aircraft engines - sudden/rapid cooling
Replies
9
Views
2K
Choosing the Right Turboprop Engine for Light Aircraft
Replies
3
Views
3K
Fixed wing aircraft control via engine gimble
Replies
3
Views
2K
How to Approximate Aerodynamic Coefficients? (Lift/Drag)
Replies
1
Views
3K
Static Stability of Aircraft designed in X Plane
Replies
1
Views
4K

Hot Threads

Recent Insights

Back
Top