JPH0433198Y2 - - Google Patents

Info

Publication number
JPH0433198Y2
JPH0433198Y2 JP15727486U JP15727486U JPH0433198Y2 JP H0433198 Y2 JPH0433198 Y2 JP H0433198Y2 JP 15727486 U JP15727486 U JP 15727486U JP 15727486 U JP15727486 U JP 15727486U JP H0433198 Y2 JPH0433198 Y2 JP H0433198Y2
Authority
JP
Japan
Prior art keywords
static pressure
aircraft
thin plate
pressure hole
guide
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP15727486U
Other languages
English (en)
Japanese (ja)
Other versions
JPS6363300U (en)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP15727486U priority Critical patent/JPH0433198Y2/ja
Publication of JPS6363300U publication Critical patent/JPS6363300U/ja
Application granted granted Critical
Publication of JPH0433198Y2 publication Critical patent/JPH0433198Y2/ja
Expired legal-status Critical Current

Links

Landscapes

  • Medicinal Preparation (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
JP15727486U 1986-10-14 1986-10-14 Expired JPH0433198Y2 (en))

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15727486U JPH0433198Y2 (en)) 1986-10-14 1986-10-14

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15727486U JPH0433198Y2 (en)) 1986-10-14 1986-10-14

Publications (2)

Publication Number Publication Date
JPS6363300U JPS6363300U (en)) 1988-04-26
JPH0433198Y2 true JPH0433198Y2 (en)) 1992-08-10

Family

ID=31079666

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15727486U Expired JPH0433198Y2 (en)) 1986-10-14 1986-10-14

Country Status (1)

Country Link
JP (1) JPH0433198Y2 (en))

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2891368B1 (fr) * 2005-09-27 2007-11-30 Airbus France Sas Systeme de surveillance de parametres anemobaroclinometriques pour aeronefs

Also Published As

Publication number Publication date
JPS6363300U (en)) 1988-04-26

Similar Documents

Publication Publication Date Title
US4907970A (en) Sidestick-type thrust control simulator
US5627311A (en) Transportable three-dimensional calibration wind tunnel system, verification method of flight control system and flight simulator using same
Harris THE 7 BY 10 FOOT WIND TUNNEL OF THE NATIONAL ADVISORY COMMITTEE
JP2000131186A (ja) 風洞シミュレーション装置及び該風洞シミュレーション装置を用いた機体設計方法
CN111561543A (zh) 一种掘进机惯导组合定位装置减振系统及其使用方法
JPH0433198Y2 (en))
Wehrend Jr et al. Flight tests of the total automatic flight control system (TAFCOS) concept on a DHC-6 Twin Otter aircraft
Curry et al. Ground-effect characteristics of the Tu-144 supersonic transport airplane
Kelly et al. Flight investigation of manual and automatic vtol decelerating instrument approaches and landings
CN113581489A (zh) 一种飞机操纵面静平衡矩调节装置和调节方法
Antoniewicz et al. User's manual for interactive LINEAR: A FORTRAN program to derive linear aircraft models
JPS61175541A (ja) 風洞試験計測装置
LIU et al. The acoustic results of a United Techologies scale model helicopter rotor tested at DNW
Tosti et al. Hovering Flight Tests of a Four-Engine-Transport Vertical Take-Off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream
Jackson Jr et al. Validation of a research simulator for investigating jet transport handling qualities and airworthiness criteria during takeoff
JPH03296635A (ja) 風洞
Faber Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking
JPH04325395A (ja) 航空機
Assadourian Ground Simulator Studies of a Small Side-located Controller in a Power Control System
Robertson et al. A semi-captive trajectory system for the FSU polysonic wind tunnel
SEACORD JR Application of Frequency-Response Analysis to Aircraft-Autopilot Stability
KREISSELMEIER et al. An in-flight controller insensitive to parameters variation
Seibel Periodic Aerodynamic Forces on Rotors in Forward Flight
Tomlinson et al. Further piloted simulation studies of the handling characteristics of a slender-wing supersonic transport aircraft during approach and landing
Webster A single axis study of flight simulator kinematics by difference techniques