A simple graphical solution for rocket wake boundaries

Details A simple graphical solution for rocket wake boundaries A simple graphical solution for rocket wake boundaries

Oct 1973

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1973p%26ss...21.1625s&link_type=abstract

Planetary and Space Science, Volume 21, Issue 10, p. 1625-1632.

Computer Science

Sound

Scientific paper

Assuming a simple conical `aerodynamic' wake extending downstream from any point on the surface of a sounding rocket of typical configuration, equations are given to calculate whether a boom-mounted probe is within the wake, for varying wake angles. The calculation is straightforward for wake angles 0° and 90°. For the general case, as an alternative to solving quartic equations, a simple graphical method of solution is provided, affording quick solutions in generalized coordinates applicable to a wide range of rocket and boom configurations. Now at the General Electric Company, Lynn, Massachusetts, U.S.A.

Affiliated with

Also associated with

No associations

Rating

A simple graphical solution for rocket wake boundaries does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with A simple graphical solution for rocket wake boundaries, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and A simple graphical solution for rocket wake boundaries will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1510377