Author: Roland E. OlsonPublisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 88
Book Description
An Aerodynamic and Hydrodynamic Investigation of Two Multi-jet Water-based Aircraft Having Low Transonic Drag Rise
Author: Roland E. OlsonPublisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 88
Book Description
Aerodynamic and Hydrodynamic Characteristics of a Proposed Supersonic Multijet Water-based Hull-type Airplane with a Variable-incidence Wing
Author: William W. PetyniaPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 94
Book Description
Aerodynamic and Hydrodynamic Characteristics of a Model of a 500,000-pound High-subsonic Multijet Logistics Transport Seaplane
Author: Walter J. KapryanPublisher:
ISBN:
Category :
Languages : en
Pages : 116
Book Description
NASA Technical Memorandum
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 416
Book Description
NASA Memorandum
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 496
Book Description
NASA Technical Note
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 580
Book Description
Transonic Aerodynamic Characteristics of a Model of a Proposed Six-engine Hull-type Seaplane Designed for Supersonic Flight
Author: Dewey E. WornomPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 42
Book Description
An Investigation of the Hydrodynamic Characteristics of a Dynamic Model of a Transonic Seaplane Design Having a Planing-tail Hull
Author: Archibald E. Morse (Jr.)Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation was made of the hydrodynamic characteristics of a 1/17-size dynamic model of a 160,000-pound transonic seaplane design having a planing-tail hull with the center of gravity located 2.1 beams aft of the step. Longitudinal stability during smooth-water take-off and landing was satisfactory, and the landing behavior in waves was good. These results were similar to that of a previously tested planing-tail-hull model having the center of gravity slightly aft of the step. The thrust from currently available engines was sufficient to accelerate to take-off in 20 seconds in a distance of 2,530 feet (full-size) with a gross load of 160,000 pounds, and in 34 seconds in a distance of 4,320 feet with a gross load of 200,000 pounds. Spray characteristics were very good in smooth water and in waves.
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 218
Book Description
