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Public Domain Aeronautical Software (PDAS)
List of Difficult Problems
The current list of difficult questions:
(The ones that do not have links are not ready for posting yet.)
As noted previously, you may not be able to display the XHTML version
unless your browser is up-to-date and you have the math fonts.
See page http://www.pdas.com/ralph/mathml.html for help.
Why doesn't the atmosphere fall to the ground?
XHTML, 6KB
How thick is the earth's atmosphere?
XHTML, 6KB
What is geopotential altitude?
XHTML+MathML, 6KB or
PDF, 42KB .
What are the equations of hydrostatic equilibrium?
PDF, 50KB
What is the surface area of a Sears-Haack body?
XHTML+MathML, 6KB or
PDF, 46KB
How do you compute the wave angle for a given Mach and
deflection angle in an oblique shock?
XHTML+MathML, 5KB or
PDF, 42 KB
How do you compute the trajectory of a baseball in air?
XHTML, 8KB
How do you compute the inverse of the Prandtl-Meyer function?
XHTML+MathML, 5KB or
PDF, 44KB
What is the difference between a Sears-Haack body and a
Von Karman Ogive?
What is the wave drag coefficient of a body of revolution
defined by the radius at a finite set of points?
What is the supersonic area rule?
What is the induced drag coefficient of a wing whose local
lift coefficient is known at a finite set of points?
How does one compute the shape of a NACA 6-series airfoil?
What is Shock-Expansion Theory?
What is Second-Order Shock-Expansion Theory?
Get a copy of all the programs from
Public Domain Computer Programs for the Aeronautical Engineer.
Last updated: 2022 Oct 17
by Ralph Carmichael, pdaerowebmaster AT gmail DOT com
PDAS Home >
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Public Domain Aeronautical Software (PDAS)