Ramjet Ignition Airspeed: What You Need to Know

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    Ignition Ramjet
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Discussion Overview

The discussion revolves around the airspeed required to ignite a ramjet, including both the vehicle's airspeed and the airspeed within the combustion chamber. Participants explore the efficiency of ramjets, weight considerations, and the metrics used to rate their performance.

Discussion Character

  • Exploratory
  • Debate/contested
  • Technical explanation

Main Points Raised

  • One participant inquires about the specific airspeed needed for ignition in a ramjet, both for the vehicle and the combustion chamber.
  • Another participant suggests that determining the required velocity for ignition could be complex and potentially extensive to explain.
  • A participant requests detailed information regarding the airspeeds for ignition at 60% efficiency, the vehicle's weight, acceleration time to maximum efficiency, and how ramjets are rated (specific impulse vs. pounds of thrust).
  • There is a discussion about the reliability of Wikipedia as a source of information, with one participant expressing skepticism about its credibility.
  • Another participant compares Wikipedia to Physics Forums, suggesting that both can contain inaccuracies due to anonymous contributions.

Areas of Agreement / Disagreement

Participants express differing views on the reliability of Wikipedia as a source, indicating a lack of consensus on this point. The technical questions regarding ramjet ignition and efficiency remain largely unresolved, with multiple inquiries and no definitive answers provided.

Contextual Notes

The discussion does not clarify the assumptions behind the efficiency metrics or the specific conditions under which the airspeeds are to be measured. There is also no resolution on the maximum efficiency of a state-of-the-art ramjet.

joaquinwalkin
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What airspeed do I need to ignite a ramjet?
 
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Are you asking "what is the required velocity of air inside the combustion chamber in order for it to ignite with a decent efficienty?" This is a tough question, I could write an essay about it just in this post.
 
I was thinking about the airspeed of the vehicle, but both airspeeds would be appreciated (vehicle and combustion chamber). So with a state of the art ramjet what would be those speeds to ignite with 60% efficiency. And if you don't mind say the vehicle weighs 500 pounds and is carrying 1,000 pounds of fuel (1,500 pounds total weight) how long would it take it to accelerate to maximum efficiency. What is maximum efficiency for a state of the art ramjet? And are they rated in specific impulse or pounds of thrust?
Thank-you very much.
 
joaquinwalkin said:
I was thinking about the airspeed of the vehicle, but both airspeeds would be appreciated (vehicle and combustion chamber). So with a state of the art ramjet what would be those speeds to ignite with 60% efficiency. And if you don't mind say the vehicle weighs 500 pounds and is carrying 1,000 pounds of fuel (1,500 pounds total weight) how long would it take it to accelerate to maximum efficiency. What is maximum efficiency for a state of the art ramjet? And are they rated in specific impulse or pounds of thrust?
Thank-you very much.

Welcome to the PF.

Have you been doing any reading on your own so far? Here is an intro article:

http://en.wikipedia.org/wiki/Ramjet

.
 
Thanks, but I don't consider wikipedia a reliable source of information.
 
Wikipedia = Anonymous editors writing articles
PhysicsForums = Anonymous posters answering physics questions

In theory they aren't any different in terms of potential for being wrong.
 
joaquinwalkin said:
Thanks, but I don't consider wikipedia a reliable source of information.

LOL. About ramjets?

Well, what other reading have you been doing?
 

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