271![Aerodynamics and Phonology 0. Aerodynamic phonology. 1. Some observations on subglottal pressure. Aerodynamics and Phonology 0. Aerodynamic phonology. 1. Some observations on subglottal pressure.](https://www.pdfsearch.io/img/880c75699df8a88618a6e59b32cfb2b5.jpg) | Add to Reading ListSource URL: linguistics.berkeley.eduLanguage: English - Date: 2012-09-13 13:49:38
|
---|
272![Aerodynamic and Performance Measurements on a SWT[removed]Wind Turbine Aerodynamic and Performance Measurements on a SWT[removed]Wind Turbine](https://www.pdfsearch.io/img/f1021d72608cf3dc43b07b81a3f53226.jpg) | Add to Reading ListSource URL: www.nrel.govLanguage: English - Date: 2013-10-01 17:16:55
|
---|
273![Basic principles applied at creation of the Su-35 aircraft: Aerodynamic cleanness, application of the integral aerodynamic layout with a lift
Basic principles applied at creation of the Su-35 aircraft: Aerodynamic cleanness, application of the integral aerodynamic layout with a lift](https://www.pdfsearch.io/img/6b559ebe2da37ec693cc6d38fdf4e2b2.jpg) | Add to Reading ListSource URL: www.knaapo.ruLanguage: English - Date: 2009-08-31 19:04:01
|
---|
274![REPORT No. 586 AIRFOIL SECTION CHARACTERISTICS AS AFFECTED BY VARIATIONS OF THE REYNOLDS NUMBER REPORT No. 586 AIRFOIL SECTION CHARACTERISTICS AS AFFECTED BY VARIATIONS OF THE REYNOLDS NUMBER](https://www.pdfsearch.io/img/8b3235e28c0e8a1ed849c6e8fd2204fb.jpg) | Add to Reading ListSource URL: www.ae.metu.edu.trLanguage: English - Date: 2006-03-09 02:37:19
|
---|
275![Wing Taper Considerations Tapering a wing planform gives a number of significant aerodynamic and structural advantages, but it can also cause problems if overdone. Consider three AR = 10 wings of the same span and area, but different taper ratios λ = ctip /croot . When operated at some overall lift Wing Taper Considerations Tapering a wing planform gives a number of significant aerodynamic and structural advantages, but it can also cause problems if overdone. Consider three AR = 10 wings of the same span and area, but different taper ratios λ = ctip /croot . When operated at some overall lift](https://www.pdfsearch.io/img/e82457387a61d82b8fb2e01712508826.jpg) | Add to Reading ListSource URL: ocw.mit.eduLanguage: English - Date: 2013-09-29 08:11:09
|
---|
276![Comparison of CFD and wind tunnel aerodynamic forces on a mast and mainsail Comparison of CFD and wind tunnel aerodynamic forces on a mast and mainsail](https://www.pdfsearch.io/img/26141b1da29db07a1117daf4c3be95cd.jpg) | Add to Reading ListSource URL: vincent.chapin.free.frLanguage: English - Date: 2005-12-14 07:36:13
|
---|
277![1 Design and aerodynamic considerations about the civil VTOL aircraft Ray 1 Design and aerodynamic considerations about the civil VTOL aircraft Ray](https://www.pdfsearch.io/img/52dfcb5cdee5056be8fcddbad0bfea57.jpg) | Add to Reading ListSource URL: www.rayaircraft.comLanguage: English - Date: 2010-12-16 12:25:47
|
---|
278![AERODYNAMICS OF AFTERMARKET REAR SPOILER RIDHWAN BIN CHE ZAKE AERODYNAMICS OF AFTERMARKET REAR SPOILER RIDHWAN BIN CHE ZAKE](https://www.pdfsearch.io/img/e8fd8cdc9e558e54824eba4d8900bf11.jpg) | Add to Reading ListSource URL: umpir.ump.edu.myLanguage: English - Date: 2010-05-20 04:25:51
|
---|
279![Preliminary Design Studies of a Mono Tiltrotor (MTR) with Demonstrations of Aerodynamic Wing Deployment G. Douglas Baldwin* Preliminary Design Studies of a Mono Tiltrotor (MTR) with Demonstrations of Aerodynamic Wing Deployment G. Douglas Baldwin*](https://www.pdfsearch.io/img/b824ab0f7513e20a91d755881f92abc5.jpg) | Add to Reading ListSource URL: www.baldwintechnology.comLanguage: English - Date: 2009-07-08 16:03:26
|
---|
280![](https://www.pdfsearch.io/img/55725fbb2df260dad7946f1318b0a2c1.jpg) | Add to Reading ListSource URL: pdf.aiaa.orgLanguage: English - Date: 2007-06-21 15:00:10
|
---|