Author: L. Stewart Rolls
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
Book Description
The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.
Tests of a Small-scale NACA Submerged Inlet at Transonic Mach Numbers
Author: L. Stewart Rolls
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
Book Description
The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
Book Description
The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.
NACA Research Memorandum
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
An Experimental Investigation of NACA Submerged Air Inlets on a 1/5-scale Model of a Fighter Airplane
Author: Donald E. Gault
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
Book Description
Investigation of an NACA Submerged Inlet at Mach Numbers from 1.17 to 1.99
Author: Warren E. Anderson
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
Book Description
Research Abstracts
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
Book Description
An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0
Author: Richard J. Re
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 116
Book Description
Naca Conference on Aerodynamic Problems of Transonic Airplane Design
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 524
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 524
Book Description