| LDR | 02757cam a2200361Ia 4500 | ||
| 001 | 011445838 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 021028s1960 dcua b f000 0 eng d | ||
| 029 | 1 | ⊔ | ‡aDEBBG ‡bBV022064864 |
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6394961 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)50873509 |
| 040 | ⊔ | ⊔ | ‡aAD# ‡cAD# ‡dOCLCQ ‡dDEBBG |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-331 |
| 088 | ⊔ | ⊔ | ‡aNASA-TN-D-331 |
| 100 | 1 | ⊔ | ‡aAnderson, Seth B. |
| 245 | 1 | 3 | ‡aAn examination of handling qualities criteria for V/STOL aircraft / ‡cby Seth B. Anderson. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce, ‡c[1960] |
| 300 | ⊔ | ⊔ | ‡a51 p. : ‡bill. ; ‡c26 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vNASA TN D-331 |
| 500 | ⊔ | ⊔ | ‡aPrepared at the Ames Research Center, Moffett Field, Calif. |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 500 | ⊔ | ⊔ | ‡a"July 1960."--Cover. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 520 | ⊔ | ⊔ | ‡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." |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | 0 | 7 | ‡aSenkrechtstarter. ‡2swd |
| 650 | 0 | 7 | ‡aKurzstartflugzeug. ‡2swd |
| 650 | ⊔ | 0 | ‡aFlight control. |
| 650 | ⊔ | 0 | ‡aShort take-off and landing aircraft ‡xDesign. |
| 650 | ⊔ | 0 | ‡aVertically rising aircraft ‡xAerodynamics. |
| 710 | 2 | ⊔ | ‡aAmes Research Center. |
| CID | ⊔ | ⊔ | ‡a011445838 |
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| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:18:11Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6394961 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106588822 ‡sUIU ‡16394961 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106588822 ‡y1960 ‡rpd ‡qbib ‡tUS fed doc |