LEADER 03375nam 2200565 a 450 001 9910956570103321 005 20251117094602.0 010 $a1-60086-833-9 010 $a1-60086-832-0 035 $a(CKB)2550000000072705 035 $a(EBL)3111542 035 $a(SSID)ssj0000552305 035 $a(PQKBManifestationID)12223817 035 $a(PQKBTitleCode)TC0000552305 035 $a(PQKBWorkID)10539334 035 $a(PQKB)11101269 035 $a(Au-PeEL)EBL3111542 035 $a(CaPaEBR)ebr10516646 035 $a(OCoLC)922978624 035 $a(MiAaPQ)EBC3111542 035 $a(BIP)47727465 035 $a(EXLCZ)992550000000072705 100 $a19980821d1998 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 14$aThe YC-14 STOL prototype $eits design, development, and flight test : an engineer's personal view of an airplane development /$fJohn K. Wimpress, Conrad F. Newberry 205 $a1st ed. 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc1998 215 $a1 online resource (115 p.) 300 $aDescription based upon print version of record. 311 08$a1-56347-253-8 320 $aIncludes bibliographical references. 327 $a""COVER""; ""TITLE""; ""COPYRIGHT""; ""CONTENTS""; ""PREFACE""; ""I. SUMMARY""; ""II. INTRODUCTION""; ""III. BACKGROUND""; ""IV. THE RFP AND PROPOSAL""; ""V. WAITING PERIOD""; ""VI. CONFIGURATION DEVELOPMENT""; ""VII. DETAIL DESIGN AND CONSTRUCTION""; ""VIII. GROUND AND INITIAL FLIGHT TeSTS""; ""IX. FLIGHT TESTS AT EDWARDS AIR FORCE BASE""; ""X. EPILOGUE""; ""APPENDIX A: YC-14 FLIGHTTEST RESULTS""; ""APPENDIX A: YC-14 FLIGHTTEST RESULTS""; ""APPENDIX B: PROJECT PILOT'S RECOLLECTIONS OF THEYC-14 BY RAY L. MCPHERSON"" 327 $a""APPENDIX C: OBSERVATIONS OF THE AIR FORCE PROJECT TEST PILOT BY DAVID BITTENBINDER""""APPENDIX C: OBSERVATIONS OF THE AIR FORCE PROJECT TEST PILOT BY DAVID BITTENBINDER""; ""APPENDIX D: EVALUATOR'S VIEWPOINT BY ALEXANDER KENT DAVIDSON""; ""APPENDIX E: YC-14 PROGRAM; A WORKING LEVEL VIEW BY JAMES HUTTON""; ""REFERENCES/BIBLIOGRAPHY"" 330 $aThe YC-14 was an experimental aircraft, developed between 1971 and 1977, by the Boeing Company and sponsored by the US Air Force. Its basic mission was to carry large, bulky payloads into and out of short, rough dirt fields 2,000 ft long, even if an engine failed. Designed to replace the C-130, it had considerably more capability, with a large fuselage meant to carry the largest tanks, trucks and vans in use. The YC-14 configuration had a high wing and large T-tail, with the flow from the 50,000lbs thrust turbofan engines exhausted over the top of the wing and passing over the upper surface of the flaps. The flow was turned by the flaps and deflected to augment the aerodynamic lift of the configuration. It was the most efficient powered-lift system ever developed. 606 $aYC-14 (Jet transport)$xDesign and construction 615 0$aYC-14 (Jet transport)$xDesign and construction. 676 $a623.7/465 700 $aWimpress$b John K$01866608 701 $aNewberry$b Conrad F$0314165 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910956570103321 996 $aThe YC-14 STOL prototype$94474020 997 $aUNINA