1 / 11

Examples & Uses of Jets Pitot & Static Probes - Summary EML 4304L

Examples & Uses of Jets Pitot & Static Probes - Summary EML 4304L. JSF - STOVL Version. Boeing X-32 (CDP) USMC Version*. Lockheed-Martin X-35 (CDP) USMC Version*. * Images obtained from the Official US Government, DOD, JSF Site. Examples & Uses of Jets.

ranee
Download Presentation

Examples & Uses of Jets Pitot & Static Probes - Summary EML 4304L

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Examples & Uses of JetsPitot & Static Probes - SummaryEML 4304L

  2. JSF - STOVL Version Boeing X-32 (CDP) USMC Version* Lockheed-Martin X-35 (CDP) USMC Version* * Images obtained from the Official US Government, DOD, JSF Site

  3. Examples & Uses of Jets Ground Effect for a STOVL aircraft in hover

  4. F-18 Examples & Uses of Jets F22 Raptor

  5. Supersonic Inlets & Diffusers (http://www.grc.nasa.gov/WWW/K-12/airplane/lowsup.html)

  6. (Supersonic) Microjets 100 mm 400 m 50 m Pressure tap hole Human Hair 200 m Inlet pressure hole Settling chamber Micro-nozzles C-D Micro-nozzles Converging/Sonic Micro- nozzles F. S. Alvi alvi@eng.fsu.edu

  7. 100 mm Supersonic Microjets Flow Visualization Results 100 mm ; PO~ 100 Psi 200 mm ; PO~ 120 Psi 400 mm ; PO~ 120 Psi

  8. Supersonic Jets Mach 2 Rectangular Jets Sonic Round jet (0.4 mm) Vectored Rectangular Jets Mach 2 Roundvectored Jet (~30 mm)

  9. Jet Properties

  10. Flow work + kinetic energy + potential energy = constant Summary of (some) Fluids Concepts Learned in 3015C (cont’d) • Conservation of Momentum- If viscosity is neglected: Euler’s Equation • Integrate Euler’s equation along a streamline to obtain Bernoulli’s Equation It is only valid for : incompressible fluids, steady flow along a streamline, no energy loss due to friction, no heat transfer • Conservation of Energy - If energy is added, removed or lost via pumps turbines, friction, etc.then we use the energy equation or Extended Bernoulli’s Equation: Where hA , hE is work done by or on the systems, e.g turbines, pumps, etc. and hL is Frictional Head Loss where

  11. 1 2 Pitot probes • At station 1, the fluid is moving: • P1 = Pstatic OR simply Ps V1 = V • At station 2, the fluid is rest: • P2 = Ppitot OR Ptotal OR PstognationOR P0 andV2 = 0 (fluid is at rest) • Hence, Bernoulli’s Equation is reduced to:

More Related