Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 92
Book Description
1989 High-speed Civil Transport Studies
1989 High-speed Civil Transport Studies
Author: Douglas Aircraft Company. HSCT Concept Development Group
Publisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 116
Book Description
The 1989 High-Speed Civil Transport Studies
Author: National Aeronautics and Space Administration NASA
Publisher:
ISBN: 9781731260116
Category :
Languages : en
Pages : 114
Book Description
The results are presented for the Douglas Aircraft Company system studies related to high speed civil transports (HSCTs). The system studies were conducted to assess the environmental compatibility of a HSCT at a design Mach number of 3.2. Sonic boom minimization, exterior noise, and engine emissions were assessed together with the effect of a laminar flow control (LFC) technology on vehicle gross weight. The general results indicated that (1) achievement of a 90 PLdB sonic boom loudness level goal at Mach 3.2 may not be practical; (2) the high flow engine cycle concept shows promise of achieving the side line FAR Part 36 noise limit but may not achieve the aircraft range design goal of 6,500 nautical miles; (3) the rich burn/quick quench (RB/QQ) combustor concept shows promise for achieving low EINO(sub x) levels when combined with a premixed pilot stage/advanced technology high power stage duct burner in the P and W variable stream control engine (VSCE); and (4) full chord wing LFC has significant performance and economic advantages relative to the turbulent wing baseline. Unspecified Center BOUNDARY LAYER CONTROL; CIVIL AVIATION; ENVIRONMENT EFFECTS; EXHAUST EMISSION; LAMINAR BOUNDARY LAYER; SONIC BOOMS; SUPERSONIC TRANSPORTS; AIRCRAFT FUELS; BOUNDARY LAYER FLOW; COMBUSTION CHAMBERS; COMBUSTION PRODUCTS; ENGINE DESIGN; EXHAUST GASES; HIGH SPEED; NOISE POLLUTION; VARIABLE STREAM CONTROL ENGINES...
Publisher:
ISBN: 9781731260116
Category :
Languages : en
Pages : 114
Book Description
The results are presented for the Douglas Aircraft Company system studies related to high speed civil transports (HSCTs). The system studies were conducted to assess the environmental compatibility of a HSCT at a design Mach number of 3.2. Sonic boom minimization, exterior noise, and engine emissions were assessed together with the effect of a laminar flow control (LFC) technology on vehicle gross weight. The general results indicated that (1) achievement of a 90 PLdB sonic boom loudness level goal at Mach 3.2 may not be practical; (2) the high flow engine cycle concept shows promise of achieving the side line FAR Part 36 noise limit but may not achieve the aircraft range design goal of 6,500 nautical miles; (3) the rich burn/quick quench (RB/QQ) combustor concept shows promise for achieving low EINO(sub x) levels when combined with a premixed pilot stage/advanced technology high power stage duct burner in the P and W variable stream control engine (VSCE); and (4) full chord wing LFC has significant performance and economic advantages relative to the turbulent wing baseline. Unspecified Center BOUNDARY LAYER CONTROL; CIVIL AVIATION; ENVIRONMENT EFFECTS; EXHAUST EMISSION; LAMINAR BOUNDARY LAYER; SONIC BOOMS; SUPERSONIC TRANSPORTS; AIRCRAFT FUELS; BOUNDARY LAYER FLOW; COMBUSTION CHAMBERS; COMBUSTION PRODUCTS; ENGINE DESIGN; EXHAUST GASES; HIGH SPEED; NOISE POLLUTION; VARIABLE STREAM CONTROL ENGINES...
The 1989 High-speed Civil Transport Studies
The 1990 High-speed Civil Transport Studies
Scientific and Technical Aerospace Reports
NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1064
Book Description
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1064
Book Description
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1484
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1484
Book Description
Monthly Catalog of United States Government Publications
Aeronautical Technologies for the Twenty-First Century
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309047323
Category : Science
Languages : en
Pages : 314
Book Description
Prepared at the request of NASA, Aeronautical Technologies for the Twenty-First Century presents steps to help prevent the erosion of U.S. dominance in the global aeronautics market. The book recommends the immediate expansion of research on advanced aircraft that travel at subsonic speeds and research on designs that will meet expected future demands for supersonic and short-haul aircraft, including helicopters, commuter aircraft, "tiltrotor," and other advanced vehicle designs. These recommendations are intended to address the needs of improved aircraft performance, greater capacity to handle passengers and cargo, lower cost and increased convenience of air travel, greater aircraft and air traffic management system safety, and reduced environmental impacts.
Publisher: National Academies Press
ISBN: 0309047323
Category : Science
Languages : en
Pages : 314
Book Description
Prepared at the request of NASA, Aeronautical Technologies for the Twenty-First Century presents steps to help prevent the erosion of U.S. dominance in the global aeronautics market. The book recommends the immediate expansion of research on advanced aircraft that travel at subsonic speeds and research on designs that will meet expected future demands for supersonic and short-haul aircraft, including helicopters, commuter aircraft, "tiltrotor," and other advanced vehicle designs. These recommendations are intended to address the needs of improved aircraft performance, greater capacity to handle passengers and cargo, lower cost and increased convenience of air travel, greater aircraft and air traffic management system safety, and reduced environmental impacts.