Aero Performance Problem, Other Engineering

Given data for an F-4 (W=40000 lb, S=530 ft^2, Ta@sea level=35800 lb, Mach=1.5, h=20000 ft (std day), Cd0=.0224, k=.1516) find aircraft''s specific excess power in straight-and-level flight
Posted Date: 11/27/2012 12:40:44 PM | Location : United States







Related Discussions:- Aero Performance Problem, Assignment Help, Ask Question on Aero Performance Problem, Get Answer, Expert's Help, Aero Performance Problem Discussions

Write discussion on Aero Performance Problem
Your posts are moderated
Related Questions
copper and its alloys


Q. Write short note on following :             (i) Compression moulding of plastics.             (ii) Injection moulding of plastics.



Gas turbine fuel properties and specification In the earliest days of the gas turbine engine, kerosene was regarded as the most suitable fuel. It commended itself on the grounds

List three advantages and three disadvantages of open office spaces.

The closed form solutions for ?max and Mmax are given on page 16.1-276 for several axial loads. Figure C-C2.2 summarizes the results for the first benchmark problem and Figure C-C2


NAND Gate; When constructing a NAND gate using transistors as the switching devices, the output often represents the 'inversion' of the "AND" gate. Figure 4 shows an example o