Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 63
Book Description
Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane with a Triangular Wing
Author: Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack
Author: Russell W. McDearmonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
Book Description
Experimental values of the damping in roll of three triangular wings have been obtained at Mach numbers of 1.62, 1.94, 2.22, 2.41, and 2.62 over a range of angle of attack from approximately 0 to 13 degrees. The aspect ratios of the wings were 1.46, 2.31, and 3.35.
Wind-tunnel Investigation of a Tailless Triangular-wing Fighter Aircraft at Mach Numbers from 0.5 to 1.5
Author: Leslie F. LawrenceA Wind-tunnel Investigation to Evaluate the Aerodynamic Performance of Three Different Airplane Configurations Having Arrow- and Delta-wing Plan Forms at a Mach Number of 2.91
Author: James N. MuellerNASA Technical Note
Author: Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92
Author: Richard J. RePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 292
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 374
Book Description
Applied Mechanics Reviews
Author: Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap
Author: Jerry V. KirkPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Author: