AERODYNAMIC CHARACTERISTICS OF WINGS AT SUPERSONIC SPEEDS,

reportActive / Technical Report | Accession Number: AD0634865 | Open PDF

Abstract:

Contents Application of Busemanns Conical Field Method to Thin Wings, Aerodynamic Characteristics of Solid Rectangular Airfoils at Supersonic Speeds, by E. A. Bonney The Reverse Delta Planform Lift and Drag Characteristics of Delta Wings at Supersonic Speeds, by E. A. Bonney and Sectional Characteristics of Standard Airfoils, by E. A. Bonney.

Author(s):
Snow, R. M. ; Bonney, E. A.
Author Organization(s):
JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Pagination:
0067

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
Bumblebee-55
Contract/Grant Number(s):
NOrd-7386
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1_Force Support; JCA_3.2.1_Kinetic Means; JCA_1.2.5_Lessons Learned; JCA_1.2_Force Preparation; JCA_1.4.2_Health Service Delivery; JCA_1.4_Force Support; JCA_1.2.3_Educating
Modernization Areas:
Cyber
Communities of Interest:
Air Platforms
Descriptor(s):
(*WINGS, *AERODYNAMIC CHARACTERISTICS), (*SUPERSONIC FLOW, WINGS), AIRFOILS, DELTA WINGS, SUPERSONIC FLIGHT
Field(s)/Group(s):
Aerodynamics, Fluid Mechanics
Report Date:
1947 Mar 01