Typical cruising speeds and altitudes for three commercial aircraft are: 1. Dash 8: Cruising speed: 500 km/h at an altitude of 4570 m. 2. Boeing 747: Cruising speed: 978 km/h at an altitude of 9150 m. 3. Concorde: Cruising speed: 2340 km/h at an altitude of 16 600 m. Find the Mach number of these three aircraft when flying at these cruise conditions. Use the properties of the standard atmosphere. In the U.S. Standard Atmosphere, the temperature in the inner portion of the atmosphere is defined by the following equation: For altitudes, H, of from 0 m (sea-level) to 11019 m: T = 288.16 – 0.00657H Above an altitude, H, of 11 019 m: T = 216.66 The altitude, H, is measured in meters and the temperature, T, in K.

Principles of Physics: A Calculus-Based Text
5th Edition
ISBN:9781133104261
Author:Raymond A. Serway, John W. Jewett
Publisher:Raymond A. Serway, John W. Jewett
Chapter11: Gravity, Planetary Orbits, And The Hydrogen Atom
Section: Chapter Questions
Problem 1OQ
icon
Related questions
Question
Typical cruising speeds and altitudes for three commercial aircraft are:
1. Dash 8: Cruising speed: 500 km/h at an altitude of 4570 m.
2. Boeing 747: Cruising speed: 978 km/h at an altitude of 9150 m.
3. Concorde: Cruising speed: 2340 km/h at an altitude of 16 600 m.
Find the Mach number of these three aircraft when flying at these cruise conditions. Use the
properties of the standard atmosphere. In the U.S. Standard Atmosphere, the temperature in
the inner portion of the atmosphere is defined by the following equation:
For altitudes, H, of from 0 m (sea-level) to 11019 m:
T = 288.16 – 0.00657H
Above an altitude, H, of 11 019 m:
T = 216.66
The altitude, H, is measured in meters and the temperature, T, in K.
Transcribed Image Text:Typical cruising speeds and altitudes for three commercial aircraft are: 1. Dash 8: Cruising speed: 500 km/h at an altitude of 4570 m. 2. Boeing 747: Cruising speed: 978 km/h at an altitude of 9150 m. 3. Concorde: Cruising speed: 2340 km/h at an altitude of 16 600 m. Find the Mach number of these three aircraft when flying at these cruise conditions. Use the properties of the standard atmosphere. In the U.S. Standard Atmosphere, the temperature in the inner portion of the atmosphere is defined by the following equation: For altitudes, H, of from 0 m (sea-level) to 11019 m: T = 288.16 – 0.00657H Above an altitude, H, of 11 019 m: T = 216.66 The altitude, H, is measured in meters and the temperature, T, in K.
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 6 steps

Blurred answer
Knowledge Booster
Relativistic speed and time
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, physics and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Principles of Physics: A Calculus-Based Text
Principles of Physics: A Calculus-Based Text
Physics
ISBN:
9781133104261
Author:
Raymond A. Serway, John W. Jewett
Publisher:
Cengage Learning
Stars and Galaxies
Stars and Galaxies
Physics
ISBN:
9781305120785
Author:
Michael A. Seeds, Dana Backman
Publisher:
Cengage Learning
The Solar System
The Solar System
Physics
ISBN:
9781305804562
Author:
Seeds
Publisher:
Cengage
Physics for Scientists and Engineers: Foundations…
Physics for Scientists and Engineers: Foundations…
Physics
ISBN:
9781133939146
Author:
Katz, Debora M.
Publisher:
Cengage Learning