About > AllExperts  
Search for
  Main Menu Ask a Question Browse Past Answers Meet Top Experts Be an Expert Login (Experts Only)
About Us  ·  FAQ  ·  Tell Friends About Us  ·  Link To Us  ·  Free Encyclopedia  ·  Disclaimer  ·  Tech Support   
  You are here:  AllExperts > Science > Aerospace/Aviation

Category:  Aeronautical Engineering Sort By:  
NameExpertise  Status
Paul Soderman  
U.S.
View Profile
Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage. I prefer full words in full sentences. Thanks.Available
Ask A Question
View Past Answers
Rajeevlochanam B A  
India
View Profile
structural design analysis of aero gas turbine engine ; strength, life and integrity, CareersOn Vacation
returns 07/05/2008
View Past Answers
 
VOLUNTEER TO BE AN EXPERT IN THIS CATEGORY

Recent Answers
2008-07-03  Air-vent duct noise:   Dave You do need to read some of those or other books about silencers. The airflow does not go through the steel wool, it passes down an open duct with perforated walls that allow the sound to enter...
2008-06-30  retake classes?:   1. The schools that were popular at my research center were Texas A&M, Cal Poly San Luis Obispo, Virginia Tech, Iowa State, U. of Washington, MIT, Stanford, Princeton, and others I have forgotten (in...
2008-06-30  Air-vent duct noise:   Hi Dave Sorry for the tardy answer, I have been helping fight forest fires in Northern California. But I am off today, and I love your question because it relates to the work I did at NASA. Your questions...
2008-06-19  about tution fees:   Education in Europe is free for citizens; I don't know about foreigners. In the U.S., college education is expensive - on the order of $12,000 to $20,000 per year for tuition, books, and living expenses...
2008-06-10  wings:   Hi Tanner I'm curious about the design of your aircraft because conventional dirigibles don't depend on wing lift, but I assume you have something different in mind. Wing lift, L, can be calculated as...
More Answers for "Aeronautical Engineering"


Advertise on This Site | User Agreement | Privacy Policy | Kids' Privacy Policy
Copyright  © 2007 All rights reserved. AllExperts is a property of About, Inc.
The About logo, About and About.com are registered trademarks of About, Inc.