Start Over
You searched for: Keywords angles

Search Results

Cover image for Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack

Location
Access Content Online
Cover image for An evaluation of the method for determining the Whitham F-function using distributions of downwash and sidewash angles

An evaluation of the method for determining the Whitham F-function using distributions of downwash and sidewash angles

Location Call # Status
Joyner - Fed Docs Stacks ASK AT REFERENCE DESK ✔ Available
Cover image for Table of differences of altitude to nearest foot for angles from 1 minute to 2 degrees and for distances under 1 mile

Table of differences of altitude to nearest foot for angles from 1 minute to 2 degrees and for distances under 1 mile

  • 1891
  • Format: Microform
Location Call # Status
Joyner - Microforms B300 CIS US EXEC MF I1902X-2 ✔ Available
Cover image for Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01

Location
Access Content Online
Cover image for Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊

Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊

Location
Access Content Online
Cover image for Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50

Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50

Location Call # Status
Joyner - Microforms B300 NAS 1.15:4640 ✔ Available
Cover image for Evaluation of a flow direction probe and a pilot-static probe on the F-14 airplane at high angles of attack and sideslip

Evaluation of a flow direction probe and a pilot-static probe on the F-14 airplane at high angles of attack and sideslip

Location
Access Content Online
Cover image for Some aerodynamic and control studies of lifting reentry configurations at angles of attack up to 90° at a mach number of 2.91

Some aerodynamic and control studies of lifting reentry configurations at angles of attack up to 90° at a mach number of 2.91

Location
Access Content Online
Cover image for Electric welding on seaplane derrick No. 4, built at Navy Yard, Mare Island, Calif.; Water gauges for use in determining angles of heel during inclining experiments

Electric welding on seaplane derrick No. 4, built at Navy Yard, Mare Island, Calif.; Water gauges for use in determining angles of heel during inclining experiments

  • 1923
  • Format: Microform
Location Call # Status
Joyner - Microforms B300 CIS US EXEC MF N4.3-1.27 ✔ Available
Cover image for Experimental and theoretical study of aerodynamic characteristics of some lifting bodies at angles of attack from -10° to 53° at Mach numbers from 2.30 to 4.62

Experimental and theoretical study of aerodynamic characteristics of some lifting bodies at angles of attack from -10° to 53° at Mach numbers from 2.30 to 4.62

Location Call # Status
Joyner - Microforms B300 NAS 1.15:4528 ✔ Available