000 | 00653nam a22001817a 4500 | ||
---|---|---|---|
005 | 20200218115922.0 | ||
008 | 200218b xxu||||| |||| 00| 0 eng d | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
100 | _aTaylor, Robert T. | ||
245 |
_aAn experimental investigation to determine the efffect of speed brake position on the longitudinal stability and trim of swept-Wing fighter airplane [NASA TN D-246] _cRobert T. Taylor |
||
260 |
_aWashingto, D. C. _bNASA _cFebruary 1960 |
||
300 | _a46p | ||
440 | _aNational Aeronautics and Space Administration (NASA) | ||
505 | _aTEchnical note D-246 | ||
650 | _aFighter airplane | ||
942 | _cREF | ||
999 |
_c561370 _d561370 |