Author:
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 576
Book Description
Proceedings of the Joint Symposium on Environmental Effects on VTOL Designs
SIPRE Report
International Aerospace Abstracts
NASA Technical Note
NASA SP.
Aircraft Crash Survival Design Guide: Aircraft structural crashworthiness
Aircraft Crash Survival Design Guide: Design criteria and checklists
An Analysis of the Stability and Control Characteristics of an Ejector Wing V/STOL During Transition
Author: George Kurylowich
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 212
Book Description
An analysis was performed to investigate the longitudinal stability and control characteristics of an ejector wing configuration V/STOL in transition. A derivative approach was used to obtain dynamic responses about specified trim speeds, and analysis of these responses provided an insight into the significant characteristics that might affect the pilot's control over the aircraft. The thrust levels necessary to meet the control requirements specified in MIL-F-83300 for a Level 1 category vehicle were determined as well. A similar study was made for a stowable rotor configuration, and results for the stowable rotor V/STOL and the ejector wing configuration were compared. Finally, the downwash characteristics of the ejector wing configuration were evaluated in terms of their effect on ground equipment and personnel. Spray generation during hover over water is also discussed.
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 212
Book Description
An analysis was performed to investigate the longitudinal stability and control characteristics of an ejector wing configuration V/STOL in transition. A derivative approach was used to obtain dynamic responses about specified trim speeds, and analysis of these responses provided an insight into the significant characteristics that might affect the pilot's control over the aircraft. The thrust levels necessary to meet the control requirements specified in MIL-F-83300 for a Level 1 category vehicle were determined as well. A similar study was made for a stowable rotor configuration, and results for the stowable rotor V/STOL and the ejector wing configuration were compared. Finally, the downwash characteristics of the ejector wing configuration were evaluated in terms of their effect on ground equipment and personnel. Spray generation during hover over water is also discussed.
Passenger Noise Environments of Enclosed Transportation Systems
Author: United States. Office of Noise Abatement and Control
Publisher:
ISBN:
Category : Noise
Languages : en
Pages : 164
Book Description
Publisher:
ISBN:
Category : Noise
Languages : en
Pages : 164
Book Description
Paper
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 868
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 868
Book Description