An examination of handling qualities criteria for V/STOL aircraft:
"A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington, DC
National Aeronautics and Space Administration
1960
|
| Schriftenreihe: | NASA technical note
D-331 |
| Schlagworte: | |
| Zusammenfassung: | "A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach." |
| Beschreibung: | 51 S. |
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| 246 | 1 | 3 | |a An examination of handling qualities criteria for VSTOL aircraft |
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| 490 | 1 | |a NASA technical note |v D-331 | |
| 520 | 3 | |a "A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach." | |
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| id | DE-604.BV022064864 |
| illustrated | Not Illustrated |
| index_date | 2024-07-02T16:13:42Z |
| indexdate | 2024-07-09T20:50:05Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-015279634 |
| oclc_num | 50873509 |
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| owner_facet | DE-706 |
| physical | 51 S. |
| publishDate | 1960 |
| publishDateSearch | 1960 |
| publishDateSort | 1960 |
| publisher | National Aeronautics and Space Administration |
| record_format | marc |
| series | NASA technical note |
| series2 | NASA technical note |
| spelling | Anderson, Seth B. Verfasser aut An examination of handling qualities criteria for V/STOL aircraft by Seth B. Anderson An examination of handling qualities criteria for VSTOL aircraft Washington, DC National Aeronautics and Space Administration 1960 51 S. txt rdacontent n rdamedia nc rdacarrier NASA technical note D-331 "A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach." Flight control Short take-off and landing aircraft Design Vertically rising aircraft Aerodynamics Senkrechtstarter (DE-588)4077369-3 gnd rswk-swf Kurzstartflugzeug (DE-588)4123595-2 gnd rswk-swf Senkrechtstarter (DE-588)4077369-3 s DE-604 Kurzstartflugzeug (DE-588)4123595-2 s NASA technical note D-331 (DE-604)BV021854105 331 |
| spellingShingle | Anderson, Seth B. An examination of handling qualities criteria for V/STOL aircraft NASA technical note Flight control Short take-off and landing aircraft Design Vertically rising aircraft Aerodynamics Senkrechtstarter (DE-588)4077369-3 gnd Kurzstartflugzeug (DE-588)4123595-2 gnd |
| subject_GND | (DE-588)4077369-3 (DE-588)4123595-2 |
| title | An examination of handling qualities criteria for V/STOL aircraft |
| title_alt | An examination of handling qualities criteria for VSTOL aircraft |
| title_auth | An examination of handling qualities criteria for V/STOL aircraft |
| title_exact_search | An examination of handling qualities criteria for V/STOL aircraft |
| title_exact_search_txtP | An examination of handling qualities criteria for V/STOL aircraft |
| title_full | An examination of handling qualities criteria for V/STOL aircraft by Seth B. Anderson |
| title_fullStr | An examination of handling qualities criteria for V/STOL aircraft by Seth B. Anderson |
| title_full_unstemmed | An examination of handling qualities criteria for V/STOL aircraft by Seth B. Anderson |
| title_short | An examination of handling qualities criteria for V/STOL aircraft |
| title_sort | an examination of handling qualities criteria for v stol aircraft |
| topic | Flight control Short take-off and landing aircraft Design Vertically rising aircraft Aerodynamics Senkrechtstarter (DE-588)4077369-3 gnd Kurzstartflugzeug (DE-588)4123595-2 gnd |
| topic_facet | Flight control Short take-off and landing aircraft Design Vertically rising aircraft Aerodynamics Senkrechtstarter Kurzstartflugzeug |
| volume_link | (DE-604)BV021854105 |
| work_keys_str_mv | AT andersonsethb anexaminationofhandlingqualitiescriteriaforvstolaircraft |