Read Anywhere and on Any Device!

Special Offer | $0.00

Join Today And Start a 30-Day Free Trial and Get Exclusive Member Benefits to Access Millions Books for Free!

Create Free Account

Quick and Easy Sign Up!

It takes less then 1 minute to sign up, then you can enjoy Unlimited eBooks.

Sign Up Browse

Read Anywhere and on Any Device!

  • Download on iOS
  • Download on Android
  • Download on iOS

Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness

Kenneth Margolis
4.9/5 (20832 ratings)
Read Now Download Now ⏭ listen AudioBook
Description:Wave drag equations are derived for rhombic-profile tapered wings with maximum-thickness line swept less than the Mach line. Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined. Calculations are presented for representative plan forms and for a family of wings having equal root bending stress.We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness. To get started finding Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
724
Format
PDF, EPUB & Kindle Edition
Publisher
—
Release
1948
ISBN
BX5DAQAAIAAJ

Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness

Kenneth Margolis
4.4/5 (1290744 ratings)
Read Now Download now ⏭ listen AudioBook
Description: Wave drag equations are derived for rhombic-profile tapered wings with maximum-thickness line swept less than the Mach line. Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined. Calculations are presented for representative plan forms and for a family of wings having equal root bending stress.We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness. To get started finding Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
724
Format
PDF, EPUB & Kindle Edition
Publisher
—
Release
1948
ISBN
BX5DAQAAIAAJ

More Books

Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds / by Percy J.Bobbitt Frank S. Malvestuto Jr. and Kenneth Margolis. 1956 [Leather Bound]

Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds / by Percy J.Bobbitt Frank S. Malvestuto Jr. and Kenneth Margolis. 1956 [Leather Bound]

4.4/5 (1,282,506 ratings)

Some Remarks on an Approximate Method of Estimating the Wave Drag Due to Thickness at Supersonic Speeds of Three-Dimensional Wings With Arbitrary Profile

Some Remarks on an Approximate Method of Estimating the Wave Drag Due to Thickness at Supersonic Speeds of Three-Dimensional Wings With Arbitrary Profile

4.2/5 (4,466 ratings)

Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift

Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift

4.1/5 (1,751 ratings)

Theoretical Calculations of the Lateral Force and Yawing Moment Due to Rolling at Supersonic Speeds for Sweptback Tapered Wings With Streamwise Tips. Subsonic Leading Edges

Theoretical Calculations of the Lateral Force and Yawing Moment Due to Rolling at Supersonic Speeds for Sweptback Tapered Wings With Streamwise Tips. Subsonic Leading Edges

4.5/5 (743 ratings)

Effect of Chordwise Location of Maximum Thickness on the Supersonic Wave Drag of Sweptback Wings

Effect of Chordwise Location of Maximum Thickness on the Supersonic Wave Drag of Sweptback Wings

4/5 (647 ratings)

Collecting Decoys on a Shoestring

Collecting Decoys on a Shoestring

4/5 (647 ratings)

Judaism and Health: A Handbook of Practical, Professional and Scholarly Resources

Judaism and Health: A Handbook of Practical, Professional and Scholarly Resources

4.7/5 (647 ratings)

Language Beyond Postmodernism: Saying and Thinking in Gendlin Philosophy (Studies in Phenomenology and Existential Philosophy)

Language Beyond Postmodernism: Saying and Thinking in Gendlin Philosophy (Studies in Phenomenology and Existential Philosophy)

4.6/5 (647 ratings)

Studies in Phenomenology and Existential Philosophy

Studies in Phenomenology and Existential Philosophy

4.9/5 (647 ratings)
loader