NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
NACA Conference on Aerodynamic Problems of Transonic Airplane Design
Document ID
19790079919
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
August 9, 2013
Publication Date
January 1, 1947
Subject Category
Aeronautics (General)
Report/Patent Number
NACA-1947/4
NASA-TM-804-2
Accession Number
79N79427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19790079925WorkSummary of NACA submerged-inlet investigations19790079928WorkPropellers at high speeds19790079935WorkFactors affecting lateral stability and controllability19790079937WorkFlight characteristics at transonic speeds. 1: P-80A airplane investigation19790079927WorkNacelles for high critical speeds on straight and swept wings19790079939WorkCharacteristics of a triangular-winged aircraft. 1: Performance data19790079923WorkLanding characteristics of high-speed wings19790079932WorkCurrent status of longitudinal stability19790079940WorkCharacteristics of a triangular-winged aircraft. 2: Stability and control19790079936WorkLow-speed flight investigation of an airplane with sweptback wings19790079933WorkEffects of sweep on controls. 1: Effectiveness19790079929WorkSome high-speed flutter studies19790079920WorkA review of recent information relating to the drag rise of airplanes19790079924WorkNose inlets19790079921WorkAirfoil section characteristics at high subsonic speeds19790079934WorkEffects of sweep on controls. 2: Hinge moments19790079930WorkTransonic flutter of control surfaces19790079938WorkCharacteristics of a Configuration with a Large Angle of Sweepback19790079931WorkPrediction of the aerodynamic characteristics of wings of arbitrary plan form19790079926WorkInvestigation of side inlets at supersonic speeds19790079922WorkLift and drag characteristics of a wing with several angles of sweep at high subsonic speeds
No Preview Available