22.06.2015 Views

Vendetta Final Proposal Part 2 - Cal Poly

Vendetta Final Proposal Part 2 - Cal Poly

Vendetta Final Proposal Part 2 - Cal Poly

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

11 Performance<br />

11.1 Specific Excess Power Requirements<br />

Compliance with RFP specific excess power requirements is best shown using specific excess power envelopes<br />

including those required as measures of merit. Figure 11.1 shows the 1-g military specific excess power envelope. The<br />

RFP requirement of 0 ft/s at Mach 1.6 and 50,000 ft is met with 33.7 ft/s specific excess power. The 1-g maximum<br />

(afterburner) specific excess power envelope, in Figure 11.2, shows that the RFP requirement of 200 ft/s is met with a<br />

value of 212.5 ft/s. This envelope also shows that the maximum Mach number at 36,000 ft measure of merit is 2.18.<br />

The 2-g maximum specific excess power envelope, in Figure 11.3, shows that the RFP requirement of 0 ft/s is met with a<br />

value of 8.0 ft/s. This requirement is design driver for the thrust produced by the propulsion system. The 5-g maximum<br />

specific excess power envelope and maximum sustained load factor envelope required as measures of merit are shown in<br />

Figure 11.4 and Figure 11.5 respectively.<br />

70,000<br />

60,000<br />

RFP Requirement 0<br />

50,000<br />

P s = 0 ft/s<br />

Altitude (ft)<br />

40,000<br />

30,000<br />

Stall Limit<br />

50<br />

100<br />

150<br />

150<br />

200<br />

20,000<br />

10,000<br />

Flaps<br />

200<br />

300<br />

400<br />

q Limit<br />

0<br />

0 0.5 1 1.5 2 2.5<br />

Mach<br />

Figure 11.1 - 1-g Military Specific Excess Power Envelope at Maneuver Weight<br />

59

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!