Question: A rectangular wing tested in a wind tunnel as a model 30 in. by 5 in. size has an efficiency factor ul = 0.90. The

A rectangular wing tested in a wind tunnel as a model 30 in. by 5 in. size has an efficiency factor ul = 0.90. The lift slope of the model airfoil is determined to be 0.085 per degree, with the angle of zero lift at -3. If this airfoil is used on a wing having a 42 ft span and a chord of 6 ft, what lift will be developed by the wing if it is operating at an angle of attack of 6 at 100 mph? Assume standard sea-level conditions and ul =0.90 for the full scale wing

Step by Step Solution

There are 3 Steps involved in it

1 Expert Approved Answer

Step: 1 Unlock blur-text-image

Question Has Been Solved by an Expert!

Get step-by-step solutions from verified subject matter experts

Step: 2 Unlock

Step: 3 Unlock

Students Have Also Explored These Related Mathematics Questions!

Please review and critique for any errors. provide feedback \fNon-symmetrical vs Nonsymmetrical Symmetrical . In a cambered airfoil ( nonsymmetrical), the mean camber line and Symmetrical chord line...

An aircraft with a reference wing area of 174 ft and wingspan of 37.31 ft is cruising at 10,000 ft. on a standard day. The aircraft is cruising at 172 ft/s and is known to have a C = 0.4651 and CD =...

Algorithms in Artificial Intelligence (or, the old name: Introduction to Algorithmic Decision Making) Part 1 Based on slides by David Sarne and Lirong Xia Course Tentative Schedule Introduction...

U.S. Department of Transportation Federal Aviation Administration Subject: RUNWAY LENGTH REQUIREMENTS FOR AIRPORT DESIGN Advisory Circular Date: 7/1/2005 Initiated by: AAS-100 AC No: 150/5325-4B...

Figure la shows the lifting curves from a lifting line analysis of 2D airfoil, elliptical wing with aspect ra) Whic-S and elliptical wing with aspect ratio AR=10 all with the same cambered airfoil....

Figure 1b shows the induced drag coefficient (CDi) versus lifting coefficient (CL) results from lifting line analysis of three finite wings all with the same, airfoil and no geometric twist. Three...

A model aircraft with a rectangular wing is tested in sea level conditions under a wind tunnel. The velocity of the flow is 3 0 0 m / s and the wing span and chord is 3 0 ft and 1 . 5 m respectively....

In MATLAB please! + File: NE 2700 - Aircraft Sophomore D x C Part 1 Using The Approach Outli X C Get Homework Help With Chege x c File C:/Users/baltz/Downloads/AE2780_SP21_RK Project Assignment.pdf...

Figure 2 shows an uncambered, rectangular wing with span b, chord c and aspect ratio AR-b/c=10. Model this wing using a single horseshoe vortex with a constant strength F and its bound vortex at Ine...

Can I get the solution for this? Thank you 20 points A 200-kg experimental glider with a semi-span of 7 m and chord of 1m (rectangular wing) was released at a standard altitude where the temperature...

Company A has a large number of shareholders, with no single investor owning more than 50% of the outstanding shares. Company B is managed by a family who owns 60% of the outstanding shares. Both...

Use one of the many financial information sites on the Internet, such as CNBC, CNNMoney, Google Finance, or Yahoo Finance, to complete the requirements below. Some of the sites require you to enter a...

On March 1 , Bart transfers ownership of a $ 7 0 0 , 0 0 0 life insurance policy on his life that he purchased in Y 1 . How long must Bart live to avoid inclusion of the $ 7 0 0 , 0 0 0 death benefit...

ment \$ B \$ is discontinued the sales in Department A will drop by \$ 12 \\% \$. What is the financial adva \$ \\$(148,000) \$ \$ \\$(152,000) \$ \$ \\$(147,600) \$ \$ \\$(127,600) \$