Problem 1: Streamlining From dimensional analysis, we know the drag force is FD = CopAV²/2, where CD is a dimensionless coefficient of drag. The two space shuttles below have the same area A, the same velocity V, and are flying through the same air. Which has a smaller Cp and why? (<25 words)
Problem 1: Streamlining From dimensional analysis, we know the drag force is FD = CopAV²/2, where CD is a dimensionless coefficient of drag. The two space shuttles below have the same area A, the same velocity V, and are flying through the same air. Which has a smaller Cp and why? (<25 words)
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
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![**Problem 1: Streamlining**
From dimensional analysis, we know the drag force is \( F_D = C_D \rho A V^2 / 2 \), where \( C_D \) is a dimensionless coefficient of drag. The two space shuttles below have the same area \( A \), the same velocity \( V \), and are flying through the same air. Which has a smaller \( C_D \) and why? (≤25 words)
[Images: Two space shuttles are shown; the first shuttle is streamlined with a sleeker shape, and the second shuttle appears less streamlined with more surface unevenness.]
Explanation: The shuttle with the sleeker, more aerodynamic design likely has a smaller \( C_D \) due to reduced air resistance.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fc837c159-281c-429a-9ec5-8a70fc5b4137%2F9f7cb588-a022-4afa-adaf-d8af4a9e26a8%2F71965u_processed.png&w=3840&q=75)
Transcribed Image Text:**Problem 1: Streamlining**
From dimensional analysis, we know the drag force is \( F_D = C_D \rho A V^2 / 2 \), where \( C_D \) is a dimensionless coefficient of drag. The two space shuttles below have the same area \( A \), the same velocity \( V \), and are flying through the same air. Which has a smaller \( C_D \) and why? (≤25 words)
[Images: Two space shuttles are shown; the first shuttle is streamlined with a sleeker shape, and the second shuttle appears less streamlined with more surface unevenness.]
Explanation: The shuttle with the sleeker, more aerodynamic design likely has a smaller \( C_D \) due to reduced air resistance.
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