Heat transfer effects on a subsonic delta wing
With the advent of the "Space Shuttle" concept, it has become necessary to study the effects of heat transfer on the aerodynamic and boundary layer characteristics of a heated delta wing. Thus, a symmetrical 60° delta wing was tested up to twice freestream temperature in the Virginia Tech...
Main Author: | Blohm, Raymond William |
---|---|
Other Authors: | Aerospace Engineering |
Format: | Others |
Language: | en |
Published: |
Virginia Polytechnic Institute and State University
2015
|
Subjects: | |
Online Access: | http://hdl.handle.net/10919/56172 |
Similar Items
-
Modeling increased height, diameter, and specific gravity effects on yield estimates in planted loblolly pine stands
by: Tisdale, Harold Thomas
Published: (2017) -
Some economic implications of city status for Blacksburg, Virginia
by: King, Theodore Elvin
Published: (2014) -
Acquisition and retention of an active avoidance response to intense white noise: Kamin effect
by: Brett, Claude William
Published: (2015) -
Studies on the uptake and fate of hemoglobin pinocytosed by rat embryo fibroblasts cultured in normal or low magnesium media
by: Bradford, William Wills
Published: (2015) -
Flight test of a supersonic decelerator on Earth to simulate a Mars entry
by: Branscome, Darrell R.
Published: (2017)