Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
Some Recent Applications of the Suction Analogy to Vortex-lift Estimates
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 600
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 600
Book Description
Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack
Author: James M. Luckring
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 992
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 992
Book Description
Application of the Leading-edge-suction Analogy of Vortex Lift to the Drag Due to Lift of Sharp-edge Delta Wings
Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 18
Book Description
NASA Conference Publication
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 432
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 432
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 166
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 166
Book Description
Aerodynamic Analyses Requiring Advanced Computers
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 788
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 788
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 888
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 888
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Transonic Pressure Measurements and Comparison of Theory to Experiment for an Arrow-wing Configuration
Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 500
Book Description
A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings as well as a variety of leading- and trailing-edge control surface deflections, was conducted at Mach numbers from 0.4 to 1.1 to provide an experimental pressure data base for comparison with theoretical methods. Theory-to-experiment comparisons of detailed pressure distributions were made using current state-of-the-art attached and separated flow methods. The purpose of these comparisons was to delineate conditions under which these theories are valid for both flat and twisted wings and to explore the use of empirical methods to correct the theoretical methods where theory is deficient. The results are summarized.
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 500
Book Description
A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings as well as a variety of leading- and trailing-edge control surface deflections, was conducted at Mach numbers from 0.4 to 1.1 to provide an experimental pressure data base for comparison with theoretical methods. Theory-to-experiment comparisons of detailed pressure distributions were made using current state-of-the-art attached and separated flow methods. The purpose of these comparisons was to delineate conditions under which these theories are valid for both flat and twisted wings and to explore the use of empirical methods to correct the theoretical methods where theory is deficient. The results are summarized.