Recent content by sorter

An unfortunate incident happened at our triple effect caustic evaporator (32w.t% to 51w.t%). The third effect (highlighted red) where major steam (~12-13bar depending on flowrate) assisted evaporation take place, here for some reason Ni tubes get severely collapsed, while the plant was offline...

Sir, what further information should I share. I think am pretty much clear

In our electrolysis of brine, Cl2 & H2 are produced as gaseous products along with aqueous NaOH. In this scenario I require what amount of maximum moisture can Cl2 or H2 hold up at specific temperature & pressure (precisely 85celsius & 1.2bar absolute). Two coolers (shell/tube exchanger with...

Retros used for deorbital/orbital insertions..ok thnx got it. But verniers used for altitude control?...ths makes no sense in the presence of large primary nozzles which are to take care about altitude. I thing verniers are for orientation control.

these two term are different but from photos the two components looks quiet alike..i had done some search but can't grasp ACTUAL difference b/w the two as both are small rocket auxillary nozzles... by the way I have been able to discover what is in the first photo but can't identify a...

for safety measure I vote for liquid rather than solid rocket engines...atleast via a safe valve (if something goes wrong) you can put off the supply line of fuel/oxidiser

Start with this http://www.pilotbooks.co.nz/index.php?page=ourbooks&id=1 another good book free.. http://www.aerotraining.com/reference/AC61-23C-Canada.htm

^^ Thnx both of you for your contributions

regarding ambiguity b/w fences & GasterBumps(I can't find any picture. of the latter) http://en.wikipedia.org/wiki/Wing_fence Regarding 2nd question. In my understanding the pure-delta wing is highly prone to stall at high AoA reason is the spanwise flow! This problem thus can be...

YouTube - Air-Flow Characteristics on a 40 Degree Swept Back Wing the above video indicates that as the angle of attack rises the span-wise airflow rises & more probably the leading wing edges will stall first. Also notice that no appreciable change in airflow occurs at the root(attachment...

you got that right:)

for highest lift you must make something like B-2; I.e blending fuselage with wings in such a way that the whole resulting shape acts like an airfoil! http://img99.imageshack.us/img99/9771/flyingwinggoogledocs129.png Uploaded with ImageShack.us see the sideview of B-2 just like an...

There occurs various hybrid wings; however currently the most researched is Morphing Wings

Guys,, but their must be some difference b/w choosing + over x

talking about Drag parameter only; wht you suggest; either + or X configuration will have more than the other??