Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7 results returnedSearch results
- Flight Measurements of Base Pressure on Bodies of Revolution With and Without Simulated Rocket Chambers
- An Investigation of the Longitudinal Characteristics of the X-3 Configuration With Wing and Horizontal Tail Surfaces of Aspect Ratio 3.0 by Means of Rocket-Propelled Models: Results at High Lift Coefficients
- Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60©� delta wing and a high unwept horizontal tail
- Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8
- Longitudinal characteristics at transonic and supersonic speeds of a rocket-propelled airplane model having a 60-degree delta wing and low swept horizontal tail
- Flight measurements of base pressure on bodies of revolution with and without simulated rocket chambers
- Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-Sided Fuselage: Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3