Calculation of the wave drag due to lift for an arbitrary rectilinear-planform wing-body combination
no abstract provided by author === Master of Science
Main Author: | Olstad, Walter B. |
---|---|
Other Authors: | Aeronautical Engineering |
Format: | Others |
Language: | en_US |
Published: |
Virginia Polytechnic Institute
2017
|
Subjects: | |
Online Access: | http://hdl.handle.net/10919/80235 |
Similar Items
-
An analytical method for predicting lift and drag characteristics of flat-top wing-body combinations at supersonic speeds
by: Hasson, Dennis Francis
Published: (2017) -
A study of the reactions of two species of the Branchiobdellidae (Oligochaeta) to high temperatures and low oxygen tensions
by: Berry, James W. (James William)
Published: (2015) -
A theory and method of predicting the stability derivatives Clᵦ, Clᵣ, Cn𝗉, and CY𝗉 for wings of arbitrary planform in subsonic flow
by: Queijo, M. J.
Published: (2014) -
Studies on the pathology of arsanilic acid toxicity in calves
by: Mestanza, Walter
Published: (2017) -
Structural efficiency study of composite wing rib structures
by: Swanson, Gary D.
Published: (2014)