Author: John G. Lowry
Publisher:
ISBN:
Category : Seaplanes
Languages : en
Pages : 22
Book Description
A comparison was made the results obtained previously for hulls with wing interference.
Effect of Length-beam Ratio on Aerodynamic Characteristics of Flying-boat Hulls Without Wing Interference
Author: John G. Lowry
Publisher:
ISBN:
Category : Seaplanes
Languages : en
Pages : 22
Book Description
A comparison was made the results obtained previously for hulls with wing interference.
Publisher:
ISBN:
Category : Seaplanes
Languages : en
Pages : 22
Book Description
A comparison was made the results obtained previously for hulls with wing interference.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 898
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 898
Book Description
Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 512
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 512
Book Description
Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness
Author: Kenneth Margolis
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 724
Book Description
Wave drag equations are derived for rhombic-profile tapered wings with maximum-thickness line swept less than the Mach line. Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined. Calculations are presented for representative plan forms and for a family of wings having equal root bending stress.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 724
Book Description
Wave drag equations are derived for rhombic-profile tapered wings with maximum-thickness line swept less than the Mach line. Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined. Calculations are presented for representative plan forms and for a family of wings having equal root bending stress.
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Book Description
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
United States Government Publications Monthly Catalog
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1606
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1606
Book Description
A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-angle Measurements
Author: Carl Kaplan
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 252
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 252
Book Description
Technical Report
Author: Aeronautical Research Council (Great Britain)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 634
Book Description
Includes its Reports, which are also issued separately.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 634
Book Description
Includes its Reports, which are also issued separately.