For Air: y = 1.4 Question B1 a) With the aid of sketches give a clear account of the operation of convergent nozzles as a function of back pressure. In your answer clearly indicate the critical points (pressure ratios) along the pressure ratio axis. A part of the expansion of new teaching and research facilities at QMUL, a new two dimensional blow- down supersonic jet facility is going to be designed, manufactured and installed at our Whitehead Aeronautical Laboratory, Figure QB1. The design Mach number for this facility is M₁ = 2.0. b) Determine the required area ratio (Aj R=287J/kgK c) What should be the supply pressure to the nozzle (P₁) in order to have a normal shock wave at a Ax) A A₂ location at which the area ratio (- A₁ You may assume P ) for this design Mach number. A₁ A atm d) For part c, what would be the discharge mass flow rate per unit throat area? =105 N/m² and T₁ = 300K. Settling Chamber Ро To is 1.5? Convergent-Divergent Nozzle Ą A A A₁ Schematic of a Supersonic Jet Facility Figure OB1 P atm

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
icon
Related questions
Question
For Air: y = 1.4
PART B
Question B1
a) With the aid of sketches give a clear account of the operation of convergent nozzles as a function of
back pressure. In your answer clearly indicate the critical points (pressure ratios) along the pressure
ratio axis.
b) Determine the required area ratio
A part of the expansion of new teaching and research facilities at QMUL, a new two dimensional blow-
down supersonic jet facility is going to be designed, manufactured and installed at our Whitehead
Aeronautical Laboratory, Figure QB1. The design Mach number for this facility is M₁ = 2.0.
A
=
A₁ A
R=287J/kg K
A₁
location at which the area ratio (
A₁
c) What should be the supply pressure to the nozzle (P) in order to have a normal shock wave at a
Ax
=) is 1.5?
A
Settling Chamber
Po
To
for this design Mach number.
d) For part c, what would be the discharge mass flow rate per unit throat area?
You may assume P =105 N/m² and To = 300K.
atm
Convergent-Divergent Nozzle
A AX
Schematic of a Supersonic Jet Facility
Figure QB1
P
atm
Transcribed Image Text:For Air: y = 1.4 PART B Question B1 a) With the aid of sketches give a clear account of the operation of convergent nozzles as a function of back pressure. In your answer clearly indicate the critical points (pressure ratios) along the pressure ratio axis. b) Determine the required area ratio A part of the expansion of new teaching and research facilities at QMUL, a new two dimensional blow- down supersonic jet facility is going to be designed, manufactured and installed at our Whitehead Aeronautical Laboratory, Figure QB1. The design Mach number for this facility is M₁ = 2.0. A = A₁ A R=287J/kg K A₁ location at which the area ratio ( A₁ c) What should be the supply pressure to the nozzle (P) in order to have a normal shock wave at a Ax =) is 1.5? A Settling Chamber Po To for this design Mach number. d) For part c, what would be the discharge mass flow rate per unit throat area? You may assume P =105 N/m² and To = 300K. atm Convergent-Divergent Nozzle A AX Schematic of a Supersonic Jet Facility Figure QB1 P atm
Expert Solution
steps

Step by step

Solved in 6 steps with 36 images

Blurred answer
Knowledge Booster
Compressible Flow
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY